JPH05172040A - Propulsion device for flying body - Google Patents

Abstract

PURPOSE:To provide a space drive type propulsion device using space strain energy generated in the space itself as a propulsion force, while controlling the curvature component of the space with magnetic energy, by providing a flying body with a magnetic energy generation means and a magnetism control means. CONSTITUTION:A flying body 1 or a disc is formed to be, for example, elliptical, and propulsion engines 21 to 26 are respectively laid, for example, at four peripheral positions resulting from the equal division of a disc periphery, and at both center positions on the upper and lower sides of the disc. The engines 21 to 26 are so constituted that magnetic energy generation means and magnetism control means for the control thereof are arranged in such a way as corresponding to each other on a one-to-one basis. In this case, the magnetic energy generation means generates strong magnetic field, and increases the value of the curvature component of space around the body 1, thereby generating acceleration field as space strain energy. Also, the magnetism control means localizes the change of the curvature component in a quasi-antisymmetrical way and, at the same time, changes the magnetic field, for example, like a pulse for obtaining a propulsion force.

Description

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a propulsion device for a flying object (aircraft, manned rocket, spacecraft, etc.), and in particular, a space distortion generated in the space itself by controlling a curvature component of the space with strong magnetic energy. The present invention relates to a space-driven propulsion device that uses force as a propulsive force.

[0002]

2. Description of the Related Art Conventional propulsion systems for propellants include a method based on reaction of an air flow by a propeller, a method based on injection gas flow by an internal combustion engine such as a jet engine or a rocket engine, and electric propulsion based on reaction of a plasma flow and an ion flow. The method etc. are known. In the rocket propulsion system,
In addition to the chemical rocket propulsion system that has already been put into practical use, the application of electric propulsion systems (electric heating propulsion, ion propulsion, plasma propulsion, etc.), which have been put into practical use for attitude control of artificial satellites, to rocket propulsion is being considered, There are nuclear propulsion systems (nuclear thermal propulsion, nuclear fission pulse propulsion, fusion pulse propulsion, etc.) and non-chemical rocket propulsion systems (solar heating propulsion, ramjet propulsion, laser propulsion, etc.) as methods at the conceptual stage.

[0003]

However, in all of the conventional propelling systems for projectiles, the propelling method is based on the reaction thrust (momentum thrust) that injects the working substance to the rear at a high speed and generates a thrust in the forward direction by its reaction. As such, there is a certain limit to the speed that can be obtained.

That is, since the final arrival speed is theoretically determined from the injection speed of the working substance and the mass ratio, the limit of the obtained speed is low and an arbitrary high speed cannot be obtained.
For example, a chemical rocket (propelled by a jet gas flow) has a limit of several tens of km / sec, and an electric propulsion has a limit of several hundreds of km / sec. However, in terms of thrust-to-weight ratio (acceleration performance), it is about 100 for chemical rockets, but is very weak at 10 ^-5 to 10 ^-3 for electric propulsion. Therefore, the chemical rocket is the only propulsion system that can escape the 1G gravity zone of the earth, although the operating time is short depending on the fuel load.

Further, in the operation of a flying object, it is necessary to arbitrarily perform various operations such as a sudden start from an air stationary state, a sudden stop, and a right-angled turn in all directions. It is technically impossible, and if it were to be executed, it would lead to a situation in which the crew members would be destroyed due to the huge acceleration of inertial force. This is because the inertial force cannot be eliminated theoretically.

Furthermore, the generation of noise is unavoidable, which is harmful to the environment in combination with the emission to the injection gas. Especially in nuclear power promotion, the scattering of radioactivity is inevitable. Also, since the explosion of fuel is used, there is a safety problem.

Next, as is clear from rockets and space shuttles, it seems that several crew members are loaded on a huge amount of fuel, and the volume ratio occupied by the crew members is several percent. It is extremely small, about 10%, and there is a limit to the weight and volume of the object (human being, cargo, etc.) to fly.

[0008] Finally, the spacecraft is capable of navigating the outer space at high speed (several hundred km / sec to tens of thousands km / sec to quasi-light speed), and has a planet-atmosphere in any horizontal or vertical attitude. It is necessary to have both the ability to fly and take off and land easily, but it is impossible with the conventional propulsion system.

An object of the present invention is to provide a propulsion device based on a novel propulsion principle suitable for propelling a flying object, that is, controlling a curvature component of a space by strong magnetic energy to propel a space distortion force generated in the space itself. It is to provide a space-driven propulsion device that uses force.

[0010]

In order to achieve the above object, the propulsion device for a flying vehicle of the present invention has the following configuration. That is, the propulsion device for a flying vehicle according to the first aspect of the invention is a magnetic energy that generates a strong magnetic field for changing the curvature components of the inside of a flying vehicle (aircraft, manned rocket, spacecraft, etc.) and the space around the flying vehicle. Generating means; controlling the generation mode of the strong magnetic field by the magnetic energy generating means to locally control the change of the curvature component of the space in a quasi-antisymmetric manner, and to generate a spatial distortion force equivalent to gravity generated in the space. And a magnetic control means for setting the propulsive force of the flying object.

A projectile propelling apparatus according to a second aspect of the present invention is the projectile propelling apparatus according to the first aspect of the present invention; wherein the magnetic energy generating means is a spherical body made of a superconducting material which is a main superconducting magnet for generating a spherical magnetic field. The magnetic control means arranges an auxiliary superconducting magnet that generates a magnetic field of opposite polarity in a hemispherical magnetic field on one side of the main superconducting magnet, and a repetition frequency of exciting current pulses of both superconducting magnets. To control change;
It is characterized by that.

A projectile propelling apparatus according to a third aspect of the present invention is the projectile propelling apparatus according to the first aspect of the present invention; the magnetic energy generating means is a liquid metal storage container for storing a liquid metal that is a highly conductive fluid; A spherical blanket that is a container for generating a strong magnetic field; a nozzle that injects liquid metal from the liquid metal storage container into the blanket as atomized fluid particles; and a blanket that is disposed so as to face opposite wall portions of the blanket. A pair of superconducting magnets for generating an initial magnetic field; and a pair for irradiating pulsed laser light on fluid particles whose magnetic flux is frozen and which are arranged to face the blanket walls on both sides orthogonal to the arrangement direction of the pair of superconducting magnets. A laser light source; and an exhaust pump for returning the fluid particles whose magnetic flux is defrosted to the liquid metal storage container, The magnetic control means performs excitation current control for the pair of superconducting magnets, asymmetry control of the pair of laser light sources, control for repeating the process from injection of fluid particles to exhaust at high speed, and the like. It is a thing.

[0013]

Next, the operation of the projectile propelling apparatus of the present invention constructed as described above will be described. The propulsion system of the present invention is a space drive type that is not based on a reaction thrust (momentum thrust) due to gas fluid injection such as that of an ordinary jet engine or rocket engine but is based on a pressure thrust whose thrust is a pressure difference due to distortion of a space field Is the propulsion method. The outline is as follows.

In terms of continuum mechanics, the field-filling body is affected by the field quantity gradient. For example, sized particles move under the net pressure of a hydrostatic pressure gradient. As a field quantity, this quantity (hydrostatic pressure) is a function of location, and this pressure gradient is an important driving force. An object in a pressure gradient field moves under a net pressure difference. An object in the field of zero pressure remains stationary and does not move. It is assumed that this object generates a locally antisymmetric unidirectional pressure field around the object. In this state, the action of the pressure field on the space of the object and the action of the generated pressure field on the object are in equilibrium, so that there is pressure from the field, but the object cannot move.

Next, the action of pressure field generation on the space of the object is interrupted. Even if this action is instantaneously removed, the space does not instantaneously return to the original state of natural pressure 0, but it takes a finite time to return to pressure 0. That is, the space has a finite strain rate. In this finite time domain, the object and space fields are independent, the object is in the pressure field,
It moves under the pressure of the field. This pressure is equivalent to the net pressure difference in the pressure gradient. ON-O of this pressure field generation action
Continuous thrust is obtained by repeating the FF process at high speed. Energetically, the surrounding space is locally deformed by the pressure field generating action of the object, and the strain energy stored in the space in the form of strain by this displacement action is released by the momentary interruption of the pressure field generating action. , Strain energy of the space excluding some energy loss will be given to the object as kinetic energy when released. Here, the field pressure in space is a surface force generated from the curvature of space generated by a strong magnetic field.

This propulsion principle is derived from a new concept of space and a theory of mechanical structure of space determined from geometrical properties of space. That is, the “distortion” used here means a distortion defined on continuum mechanics, but the distortion of space is generated by the curvature of the space, and the curvature of the space is generated by the mass of the object or the magnetic field. Then, the distortion field of the space due to the object mass is the gravitational field. The magnetic field becomes equivalent to the gravitational field through the medium of curvature (distortion) of space.

Therefore, in the present invention, the generation mode of the strong magnetic field generated by the magnetic energy generation means is controlled by the magnetic control means so that the dynamic curvature change of the space area including the flying object becomes local, and the space itself is controlled. The propulsive force is the spatial distortion force (specifically, the force obtained from the field of the distorted space in the transition process in which the curved space returns to a flat space with zero curvature).

Therefore, this propulsion system is a kind of pressure difference propulsion system utilizing the proximity action (the concept that a direct action is received from the field) due to the strain of the space field, or the force generated by the strain of the space. Is equivalent to gravity, so it can be called a gravity propulsion method, but the thrust force penetrates the entire space including the projectile (a force that is evenly distributed inside the volume element and proportional to the mass of the volume element). Since gravity and inertial force are also volume forces), they have excellent characteristics as a propulsion system of a flying object, such as not receiving inertial force and theoretically achieving a quasi-light speed in a short time. Hereinafter, a mechanical structure of space (space distortion theory), a propulsion operation principle, and the like necessary for understanding the background of the present invention will be described.

Space Distortion Theory I. Basic Concept of Space (1) Space is an infinite continuum whose structure is determined by the framework of Riemannian geometry. There is only one undistorted natural state (flat space) in the space, and when all the external physical effects causing the distortion are removed, the space always returns to the undistorted natural state. Adjacent points in space remain as adjacent points under any physical action, and the change is continuous, and the basic condition that it is a continuum after the change is satisfied. It is a continuum in the sense that it satisfies this hypothesis. The space as a continuum is Riemann space, and its structure follows Riemannian geometry.

(2) Bending of space is a purely geometric quantity. In order to relate this geometric quantity to the actual force, the concept of strain in continuum mechanics is important. The strain field is the point of contact between the geometric quantity and the actual mechanics.

(3) Consider the local change in the geometrical structure of the space as the distortion state of the space. The change in the geometrical structure is a change in the curvature component, which indicates a transition from a flat space (Minkowski space) with a curvature component 0 to a fully curved space (Riemann space) with a curvature component. The fact that the space is bent and the space is distorted are essentially the same.

(4) The distortion of the space represents a kind of deformation of the space, and the material points filling the space are affected by the deformation of the space. An important analytical technique that associates the concept of continuum mechanics as a deformation with the concept of Riemannian geometry is vector translation. If the curvature is not 0, the result of translation of the vector varies depending on the path along the way due to the bending of the space, and the vector does not return to the initial value even if the vector goes around the closed curve on the curved surface. When the curvature is 0, this phenomenon does not occur.

(5) The material occupies an area in space in a continuous manner. Here, space and matter must be clearly distinguished. The substance fills the space and moves to occupy a region of the space. That is, the substance can move in the space, and moves in the space to fill the space.

(6) In order to maintain the continuity of the space, the moving speed of the material points filling the space does not exceed the strain speed of the space.

II. What is Riemannian geometry? Riemannian geometry is a geometry that deals with curved spaces. That is, in this paper, we focus on the curvature of the space, focusing on the four-dimensional Riemann space as a curved space. The target physical space is three spatial coordinate axes (x = x ¹ , y = x
^It is a four-dimensional Riemann space with ² , z = x ³ ) and one axis of time coordinates (w = ct = x ⁰ ). This is x ⁱ (i = 0, 1, 2,
Notated as 3).

The square of the infinitesimal distance ds between the point x ⁱ in the four-dimensional Riemann space and the two points at the adjacent point x ⁱ + dx ⁱ is given by Equation 1. g _ij is called a metric tensor, is a quantity that defines all geometric properties of space, and is generally a function of location. The starting point of Riemannian geometry is a metric tensor g _ij that defines an infinitesimal line element between two points. From the combination of g _ij , the Riemannian connection coefficient (Equation 2),
Furthermore, the Riemann curvature tensor (Formula 3) is defined, and the geometry of the entire space is determined.

[0027]

[Equation 1]

[0028]

[Equation 2]

[0029]

[Equation 3]

Next, the properties of the Riemann space are as follows. (1) In a flat (non-bending) space, all components of the Riemann curvature tensor are 0. In a curved space, the component of the Riemann curvature tensor is not zero. 1 is not 0
If so, the space is essentially curved.

(2) The necessary and sufficient condition for the space to be flat is that all 20 independent components of the Riemann curvature tensor are zero.

(3) In a flat space, the metric tensor has a constant value. In a curved space, the metric tensor is a function of location. That is, the metric tensor deviates from a flat value (Minkowski metric).

III. Basic structural formula of space ds is a line element between any two points in the spatial region I before structural deformation.
= G _i dx ⁱ , the infinitesimal distance is ds ² = g _ij d
x ⁱ dx ^j (left in FIG. 1). Then, in the spatial region II after the structural deformation of the space due to an external physical action (effect of the presence of matter or electromagnetic energy), the line element connecting the same two points in the same spatial region is newly changed and , Ds ′ = g _i ′ dx ⁱ ′, and the infinitesimal distance is ds ′ ² = g _ij ′ dx ⁱ dx ^j (right in FIG. 1). g _i ′ is the transformed and transferred basis vector g _i , and g _ij ′ is the metric tensor of the transformed coordinate system.

Since the degree of deformation can be expressed as a change in the distance between any two points, the following equation 4 is obtained.

[0035]

[Equation 4]

That is, the degree of geometrical structural deformation of space is described by the amount of change r _ij = g _ij ′ −g _ij of the metric tensor. This state of deformation can be expressed using the displacement vector u extended from the position before the deformation to the position occupied by the same coordinate point after the deformation for each point (Equations 5 and 6).

[0037]

[Equation 5]

[0038]

[Equation 6]

Using the above equation, the squared d of the transformed line element
When making a s' ^2, the equation (7).

[0040]

[Equation 7]

In Expression 7, the second-order minute term u ^k : _i u
_k : _j can be sufficiently ignored if the displacement is small. Here, the symbol ":" indicates a covariant derivative.

The covariant derivative is expressed by the equation (8) and differs from the ordinary derivative A _i , _{j by} the quantity of the second term. In a flat space, Riemann connection coefficient Γ ^r _ij = 0, so A _i : _j = A
_i , _j , that is, the covariant derivative of the first-order tensor (vector) A _i and the ordinary derivative match. In a curved space, it is usually necessary to correct the derivative, which is expressed as a covariant derivative.
Therefore, when the derivative of the field quantity is included, it is general to express it as a covariant derivative.

[0043]

[Equation 8]

Since the actual physical space can be treated as a minute displacement from the trial calculation of the order of strain, the second-order minute term can be ignored, and therefore, Equation 9 is obtained.

[0045]

[Equation 9]

On the other hand, as the concept of strain in continuum mechanics,
Since the distortion tensor e _ij is given by Expression 10, the relational expression of Expression 11 is obtained.

[0047]

[Equation 10]

[0048]

[Equation 11]

[Mathematical formula-see original document] Equation 11 is an equation showing a certain kind of deformation in the geometrical structure of space by the concept of distortion. It is shown that a strain field e _ij is generated when the metric tensor shifts from g _ij to g _ij ′ due to the presence of a substance or the like.

IV. Fundamental Equation of Space An important analysis method that associates the concept of continuum mechanics as a deformation with the concept of Riemannian geometry is the concept of vector translation. Mathematical Expression 12 is obtained by expanding the concept of vector translation on Riemann space.

[0051]

[Equation 12]

In Equation 12,

[0053]

[Outer 1]

Is the Riemann curvature tensor

[0055]

[Outside 2]

It is an antisymmetric tensor due to the property of, and becomes a rotation tensor indicating the rotation of the displacement field. When the space is curved, rotation of displacement (field) occurs in the region of the space.

Now, the above-mentioned rotation tensor and strain tensor are expressed in continuum mechanics.

[0058]

[Outside 3]

Satisfies the following differential equation (equation 13) regarding the displacement gradient in the direction perpendicular to the plane of rotation. This equation holds because the order of differentiation is reversible in a flat space.

[0060]

[Equation 13]

Then, in order to extend the differential equation of Equation 13 to the curved Riemann space, the equation needs to be modified into covariance, which is possible under the condition that Equation 14 holds, and A covariant differential equation is obtained.

[0062]

[Equation 14]

[0063]

[Equation 15]

[Mathematical formula-see original document] Next, this equation 15 shows that the displacement gradient of the rotation tensor corresponds to the difference of the displacement gradient of the strain tensor.

[0065]

[Outside 4]

[Formula 16] is obtained by formally multiplying. The relational expression (Equation 18) between the stress (field) tensor σ ^ij and the strain (field) tensor e _m1 on the continuum mechanics was used, and the fourth-order tensor was treated as a constant for the covariant derivative. As mentioned above, the symbol ":" indicates a covariant derivative.

[0067]

[Equation 16]

[0068]

[Equation 17]

[0069]

[Equation 18]

On the other hand, the volume force X ⁱ and the stress (field) tensor e ^ij are given by Equation 19 depending on the equilibrium condition in the continuum.

[0071]

[Formula 19]

Therefore, the equation 17 is the change amount ΔX ^{i of the} volume force.
Therefore, Equation 20 is obtained from Equations 16 and 17.

[0073]

[Equation 20]

Equation 20 shows that the spatial distortion force is generated by the gradient of the Riemann curvature tensor showing the bending of the space. The spatial distortion force generated here is a volume force that permeates the space and an object filling the space.

V. Structure of Space Curvature The curvature of space is determined by the Riemann curvature tensor. The Riemann curvature tensor is given by Equations 21 and 22.

[0076]

[Equation 21]

[0077]

[Equation 22]

The Riemann curvature tensor is a metric tensor.

[0079]

[Outside 5]

The structure of the space is determined by this metric tensor, since Then, the solution of this metric tensor is determined by the gravity field equation.

Further, it is a scalar curvature R and a rich tensor.

[0082]

[Outside 6]

And Riemann curvature tensor have the following relationship (Equation 23).

[0084]

[Equation 23]

Represents a material energy tensor

[0086]

[Outside 7]

When the above is applied to the gravitational field equation, the equation 24 is obtained. When this is expanded, the equation 25 is finally obtained.

[0088]

[Equation 24]

[0089]

[Equation 25]

On the other hand, the material energy tensor is given by
Given in.

[0091]

[Equation 26]

[Mathematical formula-see original document] where ρ is the rest mass density,

[0093]

[Outside 8]

Together with

[0095]

[Outside 9]

Indicates a four-dimensional velocity.

Now, assuming that the velocity of the substance is sufficiently smaller than the light velocity c, the four-dimensional velocity is given by equation 27. Therefore, the maximum component of matter energy tensor is μ =
Since ν = 0, Y ⁰⁰ is given by Equation 28.

[0098]

[Equation 27]

[0099]

[Equation 28]

Therefore, by substituting the equation 28 into the equation 25, the material energy tensor, that is, the maximum component R ^{00 of the} curvature due to the static mass density is obtained (the equation 29).

[0101]

[Equation 29]

Equation 29 shows that the static mass density ρ controls the curvature of space. The magnetic field B also controls the curvature of the space as described later. In other words, the mass density and magnetic field generate the space curvature.

Now, considering a space that can be approximated by a static and spherically symmetric Schwarzschild spacetime, the scalar curvature R is given by Equation 30.

[0104]

[Equation 30]

The Riemann curvature tensor on the Riemann space and the Gaussian curvature K on the two-dimensional subspace embedded in the Riemann space have the relationship of Expression 31. Further, the scalar curvature R and the Gaussian curvature K of Expression 32 I have a relationship. Therefore,
From Expression 31, Expression 33 is obtained for the two-dimensional Riemann space.

[0106]

[Equation 31]

[0107]

[Equation 32]

[0108]

[Expression 33]

VI. Curvature control of space by magnetic field Apply electromagnetic energy tensor to gravity field equation. In this case, the metric tensor g _ij is given by Equation 34.

[0110]

[Equation 34]

Equation 34 is an equation for determining the structure of the space due to electromagnetic energy. By multiplying Equation 34 by g _ij and transforming it, Equation 35 is obtained. From both equations, the following equation (Equation 36) is obtained. can get.

[0112]

[Equation 35]

[0113]

[Equation 36]

Antisymmetric tensor f _ij indicating the magnitude of electromagnetic field
By using the electromagnetic energy tensor M
^{Since ij} is given by Expressions 37 and 38, the value of M is obtained as follows (Expression 39).

[0115]

[Equation 37]

[0116]

[Equation 38]

[0117]

[Formula 39]

By substituting M = 3 into Equation 36,
Equation 40 is obtained.

[0119]

[Formula 40]

The rich tensor R ^ij has 10 independent components, but the main component is i = j = 0, that is, R ⁰⁰ . Therefore, Equation 41 is obtained from Equation 40.

[0121]

[Formula 41]

On the other hand, the antisymmetric tensor f _ij = -f _ji is given by the electric field E and magnetic field B in relation to Maxwell's electromagnetic equation (Equation 42).

[0123]

[Equation 42]

By substituting the equation 42 into the equations 37 and 38, the equation 43 is obtained, and finally the equation 44 is obtained. In addition,
In both equations, μ ₀ is 4π × 10 ⁻⁷ (H / m), ε ₀ is 1 / 36π × 10 ⁻⁹ (F / m), and c is 3 × 10 ⁸ (m / m).
s), B is a magnetic field (Tesla), and G is 6.672 × 10 ^-11 (N
M ² / kg ² ), R ⁰⁰ is the curvature component (1 / m ² ) of the space.

[0125]

[Equation 43]

[0126]

[Equation 44]

Equation 44 shows that the main curvature component of space is controlled by the magnetic field B. It is possible to control by the electric field E, but if E and B of the same size are 1 /
The value of 2 · ε ₀ E ² is about 1 compared with the value of 1 / 2μ ₀ · B ^2.
Since it is about 7 orders of magnitude smaller, the contribution of the electric field E to the curvature can be sufficiently ignored compared to the magnetic field E.

On the other hand, the main curvature component by the material energy tensor Y ^ij is given by equation 45.

[0129]

[Equation 45]

Since the curvature component R ⁰⁰ of the space is not related to the factor of the material energy or the electromagnetic energy tensor as its generation source, the expression 46 and the expression 47 are derived.

[0131]

[Equation 46]

[0132]

[Equation 47]

Since B ² / 2μ ₀ = W represents the energy density (J / m ³ ) of the magnetic field, it has the following relationship with the rest mass density ρ (kg / m ³ ) (Formula 48). Formula 48 guarantees the relational expression of mass and energy, E = mc ² .

[0134]

[Equation 48]

VII. Field pressure due to space curvature (surface force)
Generation Since the basic structure of the three-dimensional space is determined by the quadric surface structure, the Gaussian curvature K in the two-dimensional Riemann space gives a practical concept (Equation 49).

[0136]

[Equation 49]

By applying the film theory to this quadric surface, the following equilibrium conditional expression is obtained (Equation 50).

[0138]

[Equation 50]

In the equation 50,

[0140]

[Outside 10]

Is the film force (linear stress),

[0142]

[Outside 11]

Is the second basic metric of the curved surface, and P ³ is the vertical stress (surface force) on the curved surface.

The second basic metric of a curved surface has the following relationship between the principal curvature of the curved surface and the metric tensor (Equations 51, 5).
2).

[0145]

[Equation 51]

[0146]

[Equation 52]

Therefore, Equations 50 to 53 are obtained.

[0148]

[Equation 53]

Since α and i take a binary value with respect to the quadric surface, the expression 54 is obtained. Note that in Equation 54, K
₍₁₎ , K ₍₂₎ are the principal curvatures of the curved surface, and the principal curvature radius R ₁ ,
It is the reciprocal of R ₂ .

[0150]

[Equation 54]

Since the Gaussian curvature K is given by the equation 55, the equation 56 is obtained on the assumption that the film force N ¹ ₁ = N ² ₂ = N.

[0152]

[Equation 55]

[0153]

[Equation 56]

That is, the film force and the principal curvature on the curved surface generate a vertical stress P ³ (N / m ³ ) as a surface force on the curved surface,
The direction is toward the inside of the curved surface.

Now, let us consider a curved surface of a thin layer in a spherical mold space in which both the principal curvature radii R ₁ and R ₂ are equal to the radius R. Since the Gaussian curvature K is expressed by the equations 49 and 55, the equation 57 is obtained.
Substituting 1 / R = (R ^00/2 ) ^1/2 into the equation 56 gives the equation 58 and the equation 59 is obtained.

[0156]

[Equation 57]

[0157]

[Equation 58]

[0158]

[Equation 59]

Since the film force N in the space as the linear stress is considered to be a unique constant value under a constant condition, the expression 59
Therefore, the curvature of R ⁰⁰ generates a vertical stress P ³ as a surface force of the space inward of the curved surface. The vertical stress P ^{3 in} the inner direction of the curved surface is the pressure of the field, that is, the accumulation of a large number of curved surfaces in the area of the space forms a unidirectional pressure field.
Here, the surface force of the curved surface of the thin layer of space = the vertical pressure in the inner direction of the curved surface = the pressure of the field = −P ³ (N / m ² ) are all synonymous,
It is only the difference in perspective. The surface force field is a kind of force field and gives an acceleration to a substance in a region of space, so that a field of acceleration is generated. From the above, the curvature of the space (Curvature) is the surface force on the space itself.
To generate a unidirectional acceleration field in the spatial region.

VIII. Curvature of space and acceleration field An inward surface force is generated in the curved thin film layer itself due to the curvature of space, and an acceleration field is formed in a certain spatial region by the integration of these thin film layers. The strength α of the acceleration field and the main curvature component R ⁰⁰ of the space caused by the geometrical structure of this space are such that the curvature of the space is relatively small and the distortion field is weak, and this field is temporal. In the static case, the equations 60 and 61 are given by comparison with Newtonian dynamics.

[0161]

[Equation 60]

[0162]

[Equation 61]

[0163] Here, h ₀₀ represents a Hensa the Minkowski metric eta ₀₀ = -1 flat space and the metric tensor g ₀₀ of curved space, Equation 62, a relationship of the 63.

[0164]

[Equation 62]

[0165]

[Equation 63]

From Equations 62 and 63, the relationship between the curvature of the space and the acceleration field is Equations 64 and 65.

[0167]

[Equation 64]

[0168]

[Equation 65]

Further, from the equations 60 and 61, the equation 66 is obtained.

[0170]

[Equation 66]

Equation 66 is a distortion of space e ₀₀ (= 1/2 ·
It is shown that the distance gradient of h ₀₀ ) produces an acceleration field α. Further, it can be seen that the Riemann connection coefficient Γ ⁱ _{00, which} is a geometric quantity, corresponds to the physical quantity, which is the distortion gradient, e ₀₀ : _i .

In the Schwarzschild space-time, where space is static, the only component for which the Riemann connection coefficient Γ ⁱ ₀₀ is not 0 is the i = 3 component in the radial direction of the sphere, that is, Γ ⁱ _00. .. Therefore, R ⁰⁰ is given by Equation 67, and the acceleration α ³ = α is given by Equation 68.

[0173]

[Equation 67]

[0174]

[Equation 68]

Equation 68 shows that the acceleration α received by an object in the field of acceleration is proportional to the integral of the curvature of space.

In Newtonian mechanics, the acceleration α is given by the potential Φ: _i . Here, Φ is given by Expression 69, and since α = Φ: _i and Expression 60 result in Expression 70, h ₀₀ becomes Expression 71. Therefore, R ⁰⁰ becomes the formula 72.

[0177]

[Equation 69]

[0178]

[Equation 70]

[0179]

[Equation 71]

[0180]

[Equation 72]

On the other hand, the acceleration is obtained by the following equation (equation 73), and the value on the surface of the earth is obtained by substituting the radius and mass of the earth (equation 74).

[0182]

[Equation 73]

[0183]

[Equation 74]

The relational expression between the magnetic field and the curvature (Formula 75)
Therefore, the strength of the magnetic field that generates the curvature of space 3.42 × 10 ^-23 is 20 million Tesla.

[0185]

[Equation 75]

Next, the relationship between the curvature of space and the acceleration field will be examined. It has already been mentioned that the surface force of the spatial field generated by the curvature R ⁰⁰ of the spatial space is given by P ³ = N · (2R ⁰⁰ ) ^1/2 . The curvature R ⁰⁰ of the space on the surface of the earth is
Given by 3.42 × 10 ^-23 , the object in the space field at that point receives 1G of gravitational acceleration from the field. The value of curvature is extremely small, but it is large enough to cause 1G acceleration on the ground surface. Strictly speaking, the acceleration to the object is given by the gradient of the surface force, but the correspondence with the acceleration is approximated by the true surface force P ³ that generates the acceleration field by considering a sufficiently small local area in space. Obtained.

The curvature R ⁰⁰ of the space which produces the surface force P ³ which gives the field of acceleration of 1 G is brought about by the mass density of the earth, but the curvature of the space is also brought about by the magnetic field as described above. Curvature, as a property of space, must have the same result independent of its origin. Therefore, 1G = P ³ = N ・ (2 * 3.42 * 10 ^-23 ) ^1/2 = N ・
From (2 * 8.2 * 10 ^-38・ B ² ) ^1/2 , B = 20M Tesla
Becomes

Now, if the size of the earth remains the same and the mass becomes 100 times, that is, the density becomes 100 times, the curvature of the space on the surface is R ⁰⁰ = 3.42 * 10 ^-21 , which corresponds to the acceleration field. The strength is 100 G, and the corresponding magnetic field strength is 200 M Tesla by the same method as above. The same idea gives the following table.

[0189]

[Table 1]

Here, it should be noted that
It means that the value of the curvature R ^{00 and} the value of the acceleration α do not have a one-to-one correspondence. As can be seen from Expression 65, the curvature, that is, how much the space is curved does not correspond to the acceleration value itself, but corresponds to the degree of change in acceleration, that is, the gradient of the acceleration field.

Alternatively, from Equation 73, the acceleration corresponds to the integral of the distance of curvature, that is, the area range (Volume) of the curved space.

The comparison here is a comparison between the spherical surface of the substance called the earth and the spherical surface when the magnetic field is confined in a spherical shell. It should be noted that the strain potential as a body distribution density function satisfies the Laplace equation at the outer point of the surface of the sphere, that is, in free space, and therefore decays as a function of the distance r. The values in the table give a rough guide.

IX. Gravity and inertial force Both the magnitude of gravity and the inertial force are proportional to the mass of the volume element, permeate into each part of the body from the outside, are evenly distributed inside, and act uniformly on all internal material points. Is the force to do, and both have the property of volumetric force. Inertial force as pseudogravity is equivalent to gravity, and locally canceling gravity is a well-known fact as an equivalence principle. It has already been experienced because it is possible to temporarily achieve weightlessness by turning flight of an aircraft.

In order for all the material points in this volume element to equally act and move, the existence of a gradient of surface force (also called area force), that is, a kind of pressure difference gradient, is essential in this region. That is, in order to move not only the outer shell of the volume element itself but also the volume element's storage evenly, a surface force difference of ΔP is required as a driving force within the volume element (see FIG. 2). .. This mechanism creates an acceleration field.

If the space is assumed to be a continuum for gravity and inertial force, both strain gradients are generated, and although detailed formulas are omitted, the above-mentioned strain gradients generate the above-described surface force distance gradients. Therefore, a volume force that acts uniformly on all material points is generated, and the mechanism is exactly the same.

The essential difference between gravity and inertial force is that gravity has a curvature R ^{00 of} space, whereas inertial force does not have a curvature of space, that is, curvature R ⁰⁰ = 0. In the case of inertial force, since the curvature R ⁰⁰ = 0, the acceleration α is constant regardless of the location (Formula 76).

[0197]

[Equation 76]

However, in the case of gravity, the curvature of the space is a function of the place and is given by Expression 77. Therefore, the acceleration α is a function of the place and is not constant. In other words, with gravity, the value of acceleration changes with location. To be exact, there is a distance gradient, and the degree of change in this acceleration corresponds to the curvature, that is, how much the space is curved.

[0199]

[Equation 77]

Gravity and inertial force are discriminated by the presence or absence of curvature, but both the strain gradient due to the bending of the space and the line strain gradient of the space due to the acceleration motion of the object occur, and the surface force gradient is generated. It has the property of volumetric force.

Principle of Propulsion Operation To summarize the above description, bending of the space causes distortion of the space. The distortion force of the space penetrates and acts on the space and the object filling the space as a field. Such a space bend is generated not only by the mass of the object but also by the magnetic field. That is, the main curvature component R ⁰⁰ of the space can be controlled by the magnetic field (Formula 78). The curvature R ⁰⁰ of the space is a unidirectional pressure field in the space area including the object as the pressure of the space field.
P ³ is generated (Formula 79). An object in a unidirectional pressure field moves by receiving this pressure from the field. This pressure is equivalent to the net pressure difference experienced by an object in the pressure gradient field. This gives the driving principle of the invention.

[0202]

[Equation 78]

[0203]

[Equation 79]

That is, a strong magnetic field causes a bend in a space area near the arrangement area (propulsion section) of the magnetic energy generating means mounted on an object (flying body). However, since the action of changing the curvature of the space and the action of the distortion of the space are balanced by the static magnetic field, there is no propulsion (movement) of the flying object even if thrust is generated. Therefore, in order to propel the flying object, it is necessary to unilaterally break the equilibrium state between the action of the magnetic field on the space and the inverse action from the space, and for that purpose, the magnetic control means is mounted. At this time, the action on the space is performed in a quasi-static process while slowly maintaining the equilibrium state, and the inverse action from the space is instantaneously performed. It is important to control the rate of energy release. It is like a bow and arrow, and is gradually stored as strain energy of the elastic body, and is close to giving momentary energy to the arrow. Therefore, the reverse thrust cannot be generated when the magnetic field is generated.

The magnetic control means controls the generation mode so that the strong magnetic field generated by the magnetic energy generation means changes in a pulse shape or rotates the magnetic field (30 GHz), and the movement of the curvature component of the space is controlled. It produces a dynamic change and obtains continuous thrust from the space field to drive it.

The space has a finite strain velocity (light velocity) as a continuum, and it takes a finite time for the distorted (bent) space to return to a flat space even if the magnetic field is interrupted. .. During the transition process to return to a flat space, the projectile independently exists in the curved space field and can be propelled by the action from this space field.

That is, since the equilibrium state is broken by instantaneously interrupting the action of bending the space, during the minute time of the transition process in which the bent space returns to a flat space without bending,
The projectile is independent of the curved space field, and the projectile can be propelled by the adverse effect of the space field.

[0208] Generally, it is not possible to propel while dragging the place by the place generated by itself. In other words, unless the propellant and the place are independent, it cannot be promoted by the place. This is because the action on the field and the reaction from the field are in equilibrium. At this time, it is important in principle to delay the reaction from the action in time.

Characteristics of this projectile (1) Since the thrust is a volume force, all the material points including the projectile (spacecraft) and the occupants inside the projectile (spacecraft) receive the same force and are accelerated, so There is no action of force.

(2) Navigation such as sudden start, sudden stop, right-angled turn and zigzag turn from the stationary state in the air is possible.

(3) Since the magnetic field energy acting on the space is built into the flying object (spacecraft), it can be used for both planetary atmosphere and space navigation.

(4) The propulsion acceleration can be freely changed to several μG to 100 G by controlling the superconducting magnetic field. In other words, the navigation is stable (air stop-low speed-high speed is arbitrary).

(5) Since the thrust is proportional to the mass increase due to the speed increase, the propulsion acceleration is always constant. In addition, since the propulsion operation time is not limited, the final arrival speed of the flying object (spacecraft) is the quasi-light speed.

(6) Since it is not an internal combustion engine, noise (propeller sound, gas injection sound) and injection gas are not generated. Also,
Since it is not equipped with explosive fuel, it is highly safe.

(7) Since thrust acts on the entire space area including the flying object (spacecraft), the flying object (spacecraft) is present in the atmosphere.
Similarly, the air on the outer surface is accelerated and moves, and the occurrence of aerodynamic heating can be reduced. In other words, it only causes friction between air molecules, and the flying object (spacecraft) can move in the atmosphere at high speed (several kilometers per second to several tens of kilometers per second). However, it is expected that the highly heat-ionized air (plasma) will envelop the entire projectile (spacecraft).

(8) Regarding the shape of the flying object (spacecraft), it can be said that a sphere or an ellipsoid has the most excellent functional efficiency in view of the principle of operation and omnidirectionality.

(9) Since the space area around the flying object (spacecraft) is locally curved, the shape of the flying object (spacecraft) changes due to the gravitational lens effect, or the space between the observer on the ground and Depending on the position or distance and the azimuth angle, there may be a blind spot that cannot be seen at all.

[0218]

Embodiments of the present invention will be described below with reference to the drawings. 3A and 3B show the appearance of a flying object according to an embodiment of the present invention, FIG. 3A is a schematic top sectional view, and FIG. 3B is a schematic side sectional view.

The flying vehicle 1 according to this embodiment is made of an ellipsoidal shape, and propulsion engines (21 to 26) are provided at four outer peripheral positions which divide the outer periphery of the disk into four equal parts and at the central position of the upper and lower surfaces of the disk. There is.

Each of the propulsion engines (21 to 26) is constructed by associating the magnetic energy generating means with the magnetic control means for controlling the magnetic energy generating means in a one-to-one correspondence. Note that one magnetic control unit may be provided as a whole, and all magnetic energy generation units may be collectively controlled.

The magnetic energy generating means generates a strong magnetic field to increase the value of the curvature component of the space around the flying object 1 from 0 or a certain value to a certain value, and as will be described later, acceleration as a space distortion force. To generate a field. The magnetic control means
The change of the curvature component of the space caused by the strong magnetic energy is made quasi-antisymmetric locally, and at the same time, the magnetic field is changed in a pulse shape to obtain the propulsive force, or the rotation of the magnetic field causes the change of the space. The magnetic energy generating means is controlled so that the curvature component dynamically changes.

FIG. 4 shows a state in which the propulsion engine 24 of FIG. 3 (B) is operated. The projectile 1 receives an external force (pressure difference) P from an asymmetric strain field in space, and moves to the right (P ′) in the figure.
Direction). The same applies to other propulsion engines, and the propulsive forces in the vertical direction and in the directions orthogonal to each other in the horizontal plane are obtained, and movement of the propulsion engines in arbitrary directions can be controlled by combining these.

For example, if there are four propulsion engines as shown in FIG. 5, as shown in FIG. 6, sudden start and sudden stop from a stationary state in the air in any direction (FIG. 6 (A)), Combined navigation of horizontal movement and vertical ascent (descent) (Fig. 6
(B)), zigzag navigation (FIG. 6 (C)), and other arbitrary navigation that cannot be obtained by the conventional propulsion method.

Next, although the propulsion operation principle has been described above, in order to make it easier to understand, the practical propulsion concept will be explained first, and then the arrangement of the propulsion engine and the motion of the flying vehicle (spacecraft) in this order. The structural model of the propulsion engine that generates the property, propulsion efficiency, and quasi-antisymmetric space is described.

Conceptual Description of Propulsion Principle For example, an object in the space around the earth moves (falls) toward the center of the earth. The direct cause of the movement of the object is the action due to the distortion field due to the bending of the space around the earth, not the action of the earth itself.
However, the existence of the earth's mass (density) bends the space, so it is an indirect cause for the movement of objects.

When the object is directed toward the center of the earth, a strain field gradient is generated in the direction of the curvature of the space (perpendicular to the curved surface) generated by the mass (density) of the earth, which coincides with the direction of the center of the earth. (Fig. 7). It should be noted that the curved space and the object are independent and have no interaction.

Now, as a hypothetical experiment, it is assumed that the earth does not exist and only the space bend exists in the same region as the above in outer space. Objects in the turn of space will move in exactly the same way (Fig. 8). The curved space and the object are independent without any interaction.

This means that even if the sun disappears instantly on the earth revolving around the sun, its effect will reach the earth after 8 minutes and 32 seconds. Is the same interpretation as the fact that the sun still revolves around the sun.

The principle of this propulsion is that an object (spacecraft) in outer space artificially creates the above-mentioned unidirectional bending of space around the object and instantaneously cuts off the creating action. , To create a state of bending equivalent to the above. However, the state immediately after the generation action is turned off is a transition state in which the curved space returns to a flat space, and the curved space and the object (spacecraft) are independent in this process, and there is no interaction ( (Figure 9).

The acceleration α generated in the curved space region is given by the following formula 80 where R ⁰⁰ is the curvature, c is the light velocity, and r is the integration constant indicating the curved region.

[0231]

[Equation 80]

If the curvature of the space is uniform (constant value) in the area (FIG. 9), the acceleration α is given by equation 81 with the area length being s. Then, the curvature of the space is generated by the mass density ρ or the magnetic field B (Formula 82). In other words, the mass field or the magnetic field creates an acceleration field in the spatial region.

[0233]

[Equation 81]

[0234]

[Equation 82]

Disappearance of an object is impossible unless it is established as a virtual experiment or is actually an explosion. However, the equivalent of the disappearance of an object can be easily controlled by OFF control in a magnetic field.

In order to propel a spacecraft, a distorted surface of space as shown in FIG. 10 is ideal. That is, the region A ′ is a flat space having a curvature R ⁰⁰ = 0, and the region A is a space having an antisymmetric curvature such as a curved space (a distorted space) having a curvature R ⁰⁰ ≠ 0. .. The magnitude of the acceleration field generated in the curved space area A, that is, the acceleration α
Assuming that R ⁰⁰ is uniform, G is the universal gravitational constant, μ
It is as described above that ₀ is given as the magnetic permeability of the vacuum by Expression 83, and the field of acceleration is generated in the spatial region by the magnetic field B.

[0237]

[Equation 83]

However, practically, as shown in FIG.
Even if the distorted surface of the space is spherically symmetric with respect to the spacecraft engine, it does not affect propulsion. Within a finite time when the spacecraft moves under the thrust of the acceleration field in the region A, the distorted surface of the curved space in the region A ′ has already returned to the flat space (R ⁰⁰ ), so There is no reverse thrust due to the acceleration field.

Time τ when curved space returns to flat space
Is τ = 1 because the strain rate of the space is the light velocity c.
It is constant at / c. Further, since this thrust received from the acceleration field is a volume force equivalent to gravity and is proportional to the mass of the volume element, there is no spacecraft mass body in the area A ′ in the state of FIG. It can be seen that there is no reverse thrust from ′.

Practically, as shown in FIG. 12, a space in which the strained surface of the region A'is weaker than the strained surface of the region A, that is, (the curvature R ⁰⁰ ′ of the space of the region A ' ) <
It may be a space having a quasi-antisymmetric curvature such that (curvature R ⁰⁰ of space of region A). The space having the quasi-antisymmetric curvature is generated by controlling the magnetic field distribution in the engine of the spacecraft.

Assuming that the antisymmetrically distributed magnetic fields in the engine are B and B ′, respectively, the curvature of the space in the region A is given by the formula 84 and the curvature of the space in the region A ′ is given by the formula 85. Therefore, if B ′ = (1/10 to 1/40) × B is controlled,
The curvature R ⁰⁰ ′ of the space of the area A ′ is R ⁰⁰ ′ = (1/100
~1 / 1600) × R ⁰⁰ next, as a numerical order, R ⁰⁰ '"R ⁰⁰ to be able to quasi-anti-symmetric space.

[0242]

[Equation 84]

[0243]

[Equation 85]

Although there is no spacecraft mass body in the area A ', the acceleration α'in the area A'is the mathematical expression 86, and the acceleration α in the area A is the mathematical expression 87. From R ⁰⁰ '<< R ⁰⁰ , Α ′ << α
Then, the spacecraft can propel the quasi-antisymmetric space of FIG.

[0245]

[Equation 86]

[0246]

[Equation 87]

Further, the time τ in which the curved spaces in both the area A and the area A'return to a flat space is the same, and the space curvature during the movement of the spacecraft accelerated in the area A to the area A'is It has already disappeared, and α ′ = 0. The mass of the spacecraft (mass m) is 'no, because the majority is in the area A, with respect to the thrust f _A = m.alpha by acceleration, f _A' region A ≒
Since 0 × α ′ = 0, the reverse thrust by the area A ′ can be treated as a minute amount from the beginning.

Engine Arrangement Structure and Mobility of Spacecraft (Spacecraft) FIG. 13A shows six engines arranged as shown in FIG. 3. With this arrangement structure, movement in all directions is possible. It is possible. Operates front engine for forward, rear engine for reverse, right engine for right, left engine for left, top for ascent The engine is operated and the lower engine is operated for descent, but since the propulsion direction is a vector combination of the propulsion directions of the engine parts, the projectile can move in all directions.

For example, the left-right turn is performed as follows. Operate the front engine for 1 second at an acceleration of 100 G ≈ 1 km / s ² . After moving forward (linear motion at a constant speed), 1 second later, you are at a position of 1km. Then, the rear engine is operated for 1 second and then stopped. Move back 1km (constant linear motion) to return to the original position. Then, the left engine is operated for 1 second to move leftward at a right angle for 1 km (constant linear motion).

The engine is formed in the sphere,
As shown in FIG. 13 (B), if the type of engine is one sphere connected to two spheres (small sphere and large sphere) to form a bowling pin, the number of engines is Can be reduced. In the figure, the upper small sphere corresponds to the upper engine and the lower large sphere corresponds to the lower engine.

Even if four pin-shaped engines are arranged as shown in FIG. 13C, they can be moved in all directions. Further, even if three of the pin-shaped engines are arranged in a regular triangular shape, they can be moved in all directions by changing the engine control performance.

Structural Model of Propulsion Engine As a function of the engine, it is required to form a unidirectional surface force field as a pressure of the field of the space by giving a curvature to the space. The thin quadric surface of the space in which the surface force is generated is referred to as a distorted surface of the space. The surface force goes to the inside of this strained surface.

The curvature component of the space controlled by the magnetic field B is given by the expression 88. This strong magnetic field is a superconducting magnet confined in the shell of a perfect diamagnetic material (superconducting material) having spherical strength. Caused by. The reason for using the perfect diamagnetic material is to obtain only the curvature of the space without confining the magnetic field in the engine inside and outputting it to the external space. In the space around the engine, a spherical distortion surface is generated as a spherically symmetric field (Fig. 14).

[0254]

[Equation 88]

Since the engine receives the surface force toward its center in a spherical symmetry from the distorted surface of the space, the surface force is balanced and cannot move. However, other substances in the strain field around the engine move toward the center of the engine due to the surface force in the direction of the spherical center.

For propulsion, the engine requires the generation of an antisymmetric unidirectional strain field in the region of space. That is, the curvature R in one half of the space around the engine
⁰⁰ ≠ 0 (curved space), R ⁰⁰ = in the other half area
It is necessary to generate an antisymmetric field of 0 (flat space) by controlling the direction of the magnetic field.

Therefore, the principle structure of the magnetic energy generating means in the propulsion engine is as shown in FIG.
A main superconducting magnet 31 that generates a spherically symmetric magnetic field, and an auxiliary superconducting magnet 3 that is arranged in the hemispherical magnetic field on one side of the main superconducting magnet 31 so that the polarities of the magnetic fields are opposite.
It is composed of 2 and. Since the magnetic field required for propulsion has a value of several tens of billions of tesla, it cannot be realized by the usual magnetic field generating means, so a superconducting magnet is used.

As a result, the antisymmetric unidirectional strain field shown in FIG. 16 is generated. Since the engine receives antisymmetric surface forces, it moves in one direction toward a flat space area with zero curvature. Other substances in the space region (curvature ≠ 0) on one side of the engine also move toward the flat space region having a curvature 0. Therefore, by controlling ON / OFF of the generation of the magnetic field, the flying object (spacecraft) can be propelled.

The magnitude of the magnetic field is B ² = B · B = │
Since it is given by B│2, ^two different magnetic fields B ₁ , B
_{2. If} the synthetic magnetic field is B _T , Equation 89 is obtained. Then, when the two magnetic fields have the same magnitude, Equation 90 is obtained when the directions of the magnetic fields are forward, and Equation 91 is obtained when the directions of the magnetic fields are opposite.

[0260]

[Equation 89]

[0261]

[Equation 90]

[0262]

[Formula 91]

Propulsion Efficiency and Energy Formula Next, the propulsion efficiency of the present propulsion engine will be examined from the viewpoint of energy conversion in order to explain the magnetic control means. The conversion flow is as follows: supplied power energy (P _WE ) → superconducting magnetic field energy (E _MAG ) → space curvature (R ⁰⁰ ) → strain energy stored in space (U _STRAIN ): = engine output energy (E _NG P _WR ) →
Emission of spatial distortion energy → Effective propulsion energy (E _EFP )
+ Reactive propulsion energy (E _LOS ) + Radiant energy (E _RAD ) The efficiencies in each phase are given by equations 92 to 95,
The efficiency η of the entire engine is given by Equation 96.

[0264]

[Equation 92]

[0265]

[Equation 93]

[0266]

[Equation 94]

[0267]

[Formula 95]

[0268]

[Equation 96]

The strain energy U stored in the space
_STRAIN (engine output energy) is given by equation 97, and (effective propulsion energy + reactive propulsion energy + radiation energy) is given by equation 98.

[0270]

[Numerical Expression 97]

[0271]

[Equation 98]

In Expression 98, V ₁ and ρ ₁ are the volume and average density of the flying object, V ₂ and ρ ₂ are the volume and average density of a finite area around the flying object (atmospheric density in the atmosphere), h And ν are Planck's constant and radiant energy frequency. That is, the reactive propulsion energy means an energy loss for similarly accelerating the surrounding atmosphere because the main thrust is a volume force. Further, it is considered that not all spatial distortion energy is converted as propulsion energy, but a part thereof is emitted as radiant energy.

The overall efficiency of the engine is given by the mathematical expression 99 from the viewpoint of power.

[0274]

[Numerical expression 99]

In Expression 99, f is the volume force of the field (N /
m ³ ), V is the operating area (m ³ ), fV = F is the thrust (N), v is the propulsion speed (m / s), ν is the superconducting engine excitation cycle number,
E is the superconducting coil exciting voltage (V), I is the superconducting coil exciting current (A), and τ is the current pulse width (s).

In short, from the formula 99, the propulsion speed can be controlled by changing the engine excitation cycle number ν, and the thrust basically depends on the power EI of the power source and is controlled by changing the exciting current I.

Finally, the magnetic control means is configured to control the repetition frequency of the exciting current pulse. As a result, the magnetic field changes in a pulse shape and a dynamic change in the curvature of the space can be obtained with the ON / OFF of the magnetic field, and the flying space (spacecraft) has a flat curved space when the magnetic field is cut-off. The thrust as an action from the space field can be received in a pulsed manner at the instant of the transition process returning to a normal space and propelled.

Now, a specific example of the magnetic field generating means will be described.
This obtains a strong magnetic field by magnetic flux freezing and laser light implosion (FIG. 17, FIG. 18, FIG. 19).

First, the magnetic flux freezing will be briefly described. Magnetic flux freezing, also called magnetic field freezing, is a phenomenon in which when a highly conductive fluid moves in a magnetic field, magnetic flux (lines of magnetic force) attach to the fluid and try to move together. In principle, when there is relative motion between a highly conductive fluid and a magnetic field, a current is induced by electromagnetic induction, and this current interacts with the magnetic field to cancel the relative motion between the fluid and the magnetic field. As a result, the fluid and the magnetic field move together as if the lines of magnetic force were attached to the fluid. Since the magnetic field is attached (frozen) to the fluid, the lines of magnetic force are dragged and deformed or strengthened by the motion of the fluid.

This phenomenon is proposed as a hypothesis that explains the magnetic field of celestial bodies as a fossil mechanism. In other words, when the magnetic field lines are frozen in the gas when the star is born due to the contraction of the interstellar gas, the magnetic field lines are concentrated as the gas contracts, and the star has a poloidal magnetic field. It is estimated to be about 500 million tesla for a neutron star, which is the same as the observation result.

Now, in FIG. 17, (a) shows a state in which magnetic flux (lines of magnetic force) is frozen in the highly conductive fluid particles,
(B) shows a state in which the fluid particles contract due to the action of an external force or the like, and the lines of magnetic force also contract accordingly, and (c) shows a state in which the fluid particles further contract and become a poloidal type. Since the magnetic flux frozen in the fluid particles also performs the same contraction movement as the fluid particles contract, only the magnetic flux passage area S (m ² ) contracts and decreases while the magnetic flux φ (Wb) is preserved. Therefore, the magnetic flux density, that is, the strength of the magnetic flux B (Tesla) is B = φ / S, and its value increases and the magnetic field is concentrated.

FIG. 18 shows the principle of strong magnetic field concentration.
An initial magnetic field is applied to the sprayed good-conductivity fluid particles that have been injected in advance, and the magnetic flux is frozen. After that, the region of the fluid particles whose magnetic flux is frozen is irradiated with laser light from the four sides.
The surface of the irradiated fluid particles is heated to start jetting of plasma, and the fluid particles are recoiled by the jetting of plasma and compressed toward the center. A so-called implosion effect is achieved, and it plays a role of further increasing the contraction effect of the light pressure by the laser light. In addition,
Since the asymmetrical distribution of the magnetic field can be obtained by controlling the left and right laser light intensities (for example, the right intensity> the left intensity), according to this method, the auxiliary superconducting magnet 32 shown in FIG.
Can be unnecessary.

As described above, the fluid particles are rapidly contracted by the light pressure of the laser beam and the ablation (jetting) pressure generated by the reaction of the high temperature plasma gas, so that the magnetic flux frozen in the fluid particles is also contracted and the magnetic field is concentrated. Is achieved.

The laser light power density S (W / m ² ) is given by S = u · C, where u (Pa: = N / m ² ) is the light pressure and C is the light velocity value. Also, considering the volume ratio (1 / r) due to concentration, the laser light power density is S = u · C · (1 /
r).

Since the laser light power density currently in practical use is about 10 ¹⁷ to 10 ¹⁸ (W / m ² ), assuming that a radius ratio of 1/1000 due to concentration, the volume ratio is 1 / r. = 1/10 ⁹
Therefore, from S = 10 ¹⁷ (W / cm ² ) = 10 ²¹ (W / m ² ), the laser light pressure u becomes 30,000 trillion atmospheric pressure. Due to the light pressure including the implosion effect of the laser light, the magnetic flux frozen good-conducting fluid particles are rapidly contracted and a strong magnetic field is concentrated.

Next, FIG. 19 shows a strong magnetic field generator.
This strong magnetic field generation device includes a nozzle 42 for injecting liquid metal as a good conductive fluid into a blanket 41 as atomized fluid particles, a superconducting magglut 43 for generating an initial magnetic field (seed magnetic field) in the blanket 41, Same as 44,
A laser light source 45 that applies light pressure and implosion effect to the fluid particles whose magnetic flux is frozen in the blanket 41, the same 46, an exhaust pump 47 that exhausts the fluid particles whose magnetic flux is frozen, and a liquid metal storage container 48. This device is basically configured and is capable of continuously generating a pulse magnetic field of several tens of teslas to several tens of billions of teslas.

In FIG. 19, the initial magnetic field (seed magnetic field) is set to 5
An operation of continuously generating a pulse magnetic field of 500,000 Tesla will be described with 0 Tesla. First, a highly conductive fluid is injected from the liquid metal storage container 48 by the nozzle 42 into the blanket 41 as atomized particles. After that, the blanket 4 is placed by the upper and lower superconducting magnets (43, 44).
An initial magnetic field (50 Tesla) is generated in the space inside 1.
The magnetic field freezes on the injected fluid particles.

Next, the liquid laser is irradiated with pulsed laser light from the laser light source (45, 46). The power density of this pulsed laser light is 10 ¹⁴ W / cm ² = 10 ¹⁸ (W / m ² ). At this time, light pressure is ^{10 18/3 * 10 8 =} 3 * 10 9 Pa, equivalent to 30,000 atmospheres. And, due to the laser light implosion effect, the radius ratio is 1 /
Assuming 100, the volume ratio will be 1/10 ^6, and in consideration of this effect, the fluid particles will be contracted at a pressure of 30 billion atmospheres. In this case, since the area ratio is 1/10 ⁴ , the initial magnetic field of 50 Tesla is concentrated to the magnetic field of 50 * 10 ⁴ = 500,000 Tesla.

This magnetic field concentration process proceeds until the magnetic pressure and the laser light pressure are in equilibrium. When the pulse irradiation of the laser light is finished, the light pressure decreases, so the contracted fluid particles try to proceed to the expansion and explosion process due to the magnetic pressure.
At this point, the magnetic field generating action of the superconducting magnets (43, 44) is stopped. The fluid particles that are frozen in the magnetic flux by the magnetic field stop and remain in the blanket 41 are exhausted by the exhaust pump 47 and returned to the liquid metal storage container 48 again. In this process, degaussing action is performed if necessary.

The above process is set as one cycle and is repeated several thousand cycles per second. That is, a strong magnetic field of 500,000 Tesla is generated by continuous pulses of several KHz. Then, as described above, the intensities of the left and right laser light sources (45, 46) are controlled. That is, this device is provided with the magnetic energy generating means and the magnetic control means.

The generation of a strong magnetic field of about 500,000 tesla, which is the most viable in the existing technology, has been described above. The strength of the generated magnetic field depends on the laser light power density and the radius ratio obtained by the implosion effect. What is different can be understood from the above description.

That is, this apparatus freezes the magnetic flux of the initial magnetic field of 50 Tesla to 500 Tesla into atomized particles of the highly conductive fluid (liquid metal), and laser light (power density: 10 ¹⁴ W / cm) from the four sides. ² ~ 10 ¹⁸ W / cm ² ) By the implosion effect by irradiating, the fluid ratio of 1/100 to 1 / 10,000 in the radius ratio, therefore 1 / 10,000 to 1 / 100,000,000 in the area ratio, An initial magnetic field of 50 Tesla to 500 Tesla is 1/1
500,000 Tesla ~ 50
It is possible to generate an ultra-high magnetic field of 0,000 Tesla to 50 billion Tesla in a pulsed manner.

Moreover, since the spraying of atomized particles and the laser beam irradiation can be controlled mechanically and electrically, continuous pulse operation of several KHz can be easily performed. It should be noted that there is no need for a structure such as a liner for concentrating the magnetic field, and there is a feature that the structure is not destroyed by the giant magnetic pressure generated by the magnetic field generation.

Table 2 shows the expected main performance specifications of the flying object according to the present invention.

[0295]

[Table 2]

As a power source for generating the electric power necessary for the propulsion device, a small-sized liquid metal MHD generator (MHD generator using liquid metal as a working fluid) is used, and its heat source is used. An anti-particle annihilation reactor is used.

[0297]

As described above, according to the projectile propelling apparatus of the present invention, the propulsive force of the projectile is a volume force (spatial distortion force) equivalent to gravity penetrating the entire space area including the projectile. ), All material points including the flying body and the occupants inside the flying body will be accelerated by the same force, and there will be no action of inertial force, and the occupants will not be destroyed.

This is a propulsion method that theoretically eliminates inertial force,
Therefore, any navigation such as sudden start, sudden stop, right-angled turn, zigzag turn, V-turn, etc. is possible from a stationary state in the air.

Further, since the propulsive force is equivalent to gravity, the final velocity obtained can be theoretically close to the light velocity (quasi-light velocity).

Further, since the propulsion device of the present invention is not an internal combustion engine, it does not generate noise (propeller sound, gas injection sound, etc.) or injection gas, and can fly quietly. In addition, the navigation is stable (stationary in the air-low speed-high speed is optional), and fuel that is an explosive is not loaded, so safety is high.

In addition, since the propulsive force acts on the entire space area including the flying object, the air on the outer surface of the flying object is similarly accelerated, and the occurrence of aerodynamic heating can be reduced. In other words, it is only friction between air molecules and air molecules,
High-speed flying objects in the atmosphere (several km / s to several 100 km / s)
You can move with.

From the above, various excellent effects can be expected by combining the ability to navigate in outer space at a quasi-light speed and the ability to navigate in the atmosphere at a high speed and in an arbitrary flight pattern. It has a great effect on shortening the navigation time (for example, one-way half day to Mars).

[Brief description of drawings]

FIG. 1 is an explanatory diagram of a basic structure of a space.

FIG. 2 is an explanatory diagram of a surface force difference as a driving force.

FIG. 3 shows an appearance of a flying object according to an embodiment of the present invention,
(A) is a schematic top sectional view, and (B) is a schematic side sectional view.

FIG. 4 is an explanatory view of the principle of the spatial distortion propulsion mechanism.

FIG. 5 is a layout view of four propulsion engines.

FIG. 6 is a navigation explanatory diagram with four propulsion engines.

FIG. 7: Spatial distortion around the earth and the object M in this space
FIG.

FIG. 8 is an object M in the case where there is no mass body such as the earth and there is a unidirectional spatial distortion similar to the space around the earth.
FIG.

FIG. 9 is an explanatory diagram of a propulsion principle of the present invention.

FIG. 10 is an explanatory diagram of an ideal space distortion surface for propelling a spacecraft.

FIG. 11 is an explanatory view of a practical space distortion surface for propelling a spacecraft.

FIG. 12 is an explanatory view of a practical space distortion surface for propelling a spacecraft.

FIG. 13 is an explanatory diagram of the arrangement of propulsion engines and the motility of the spacecraft, (A) shows the case of six engines,
(B) shows the type of engine, (C) shows the case of four engines.

FIG. 14 is an explanatory diagram of a spatially strained surface formed by one superconducting magnet.

FIG. 15 is an explanatory diagram of the principle structure of the propulsion engine of the present invention.

FIG. 16 is an explanatory diagram of a spatial distortion surface formed by the propulsion engine of the present invention.

FIG. 17 is a conceptual diagram of magnetic field concentration by magnetic flux freezing,
(A) is a state diagram in which the magnetic flux is frozen in the highly conductive fluid particles,
(B) is a state diagram in which the fluid particles are contracted by the action of an external force and the magnetic flux is also contracted accordingly, and (c) is a state diagram in which the fluid particles are further contracted.

FIG. 18 is a principle explanatory diagram of a strong magnetic field generator according to an embodiment of the present invention.

FIG. 19 is a configuration block diagram of a strong magnetic field generator according to an embodiment of the present invention.

[Explanation of symbols]

 1 Flying Body 21-26 Propulsion Engine 31 Main Superconducting Magnet 32 Auxiliary Superconducting Magnet 41 Blanket 42 Nozzle 43-44 Superconducting Magnet 45-46 Laser Light Source 47 Exhaust Pump 48 Liquid Metal Storage Container

─────────────────────────────────────────────────── ───

[Procedure amendment]

[Submission date] September 25, 1992

[Procedure Amendment 1]

[Document name to be amended] Statement

[Name of item to be corrected] Full text

[Correction method] Change

[Correction content]

[Document name] Statement

Title of the invention Propulsion device for projectile

[Claims]

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a propulsion device for a flying object (aircraft, manned rocket, spacecraft, etc.), and in particular, a space distortion generated in the space itself by controlling a curvature component of the space with strong magnetic energy. The present invention relates to a space-driven propulsion device that uses force as a propulsive force.

[0002]

2. Description of the Related Art Conventional propulsion systems for propellants include a method based on reaction of an air flow by a propeller, a method based on injection gas flow by an internal combustion engine such as a jet engine or a rocket engine, and electric propulsion based on reaction of a plasma flow and an ion flow. The method etc. are known. In the rocket propulsion system,
In addition to the chemical rocket propulsion system that has already been put into practical use, the application of electric propulsion systems (electric heating propulsion, ion propulsion, plasma propulsion, etc.), which have been put into practical use for attitude control of artificial satellites, to rocket propulsion is being considered, There are nuclear propulsion systems (nuclear thermal propulsion, nuclear fission pulse propulsion, fusion pulse propulsion, etc.) and non-chemical rocket propulsion systems (solar heating propulsion, ramjet propulsion, laser propulsion, etc.) as methods at the conceptual stage.

[0003]

However, in all of the conventional propelling systems for projectiles, the propelling method is based on the reaction thrust (momentum thrust) that injects the working substance to the rear at a high speed and generates a thrust in the forward direction by its reaction. As such, there is a certain limit to the speed that can be obtained.

That is, since the final arrival speed is theoretically determined from the injection speed of the working substance and the mass ratio, the limit of the obtained speed is low and an arbitrary high speed cannot be obtained.
For example, a chemical rocket (propelled by a jet gas flow) has a limit of several tens of km / sec, and an electric propulsion has a limit of several hundreds of km / sec. However, in terms of thrust-to-weight ratio (acceleration performance), it is about 100 for chemical rockets, but is very weak at 10 ^-5 to 10 ^-3 for electric propulsion. Therefore, the chemical rocket is the only propulsion system that can escape the 1G gravity zone of the earth, although the operating time is short depending on the fuel load.

Further, in the operation of a flying object, it is necessary to arbitrarily perform various operations such as a sudden start from an air stationary state, a sudden stop, and a right-angled turn in all directions. It is technically impossible, and if it were to be executed, it would lead to a situation in which the crew members would be destroyed due to the huge acceleration of inertial force. This is because the inertial force cannot be eliminated theoretically.

Furthermore, the generation of noise is unavoidable, which is harmful to the environment in combination with the emission to the injection gas. Especially in nuclear power promotion, the scattering of radioactivity is inevitable. Also, since the explosion of fuel is used, there is a safety problem.

Next, as is clear from rockets and space shuttles, it seems that several crew members are loaded on a huge amount of fuel, and the volume ratio occupied by the crew members is several percent. It is extremely small, about 10%, and there is a limit to the weight and volume of the object (human being, cargo, etc.) to fly.

[0008] Finally, the spacecraft is capable of navigating the outer space at high speed (several hundred km / sec to tens of thousands km / sec to quasi-light speed), and has a planet-atmosphere in any horizontal or vertical attitude. It is necessary to have both the ability to fly and take off and land easily, but it is impossible with the conventional propulsion system.

An object of the present invention is to provide a propulsion device based on a novel propulsion principle suitable for propelling a flying object, that is, controlling a curvature component of a space by strong magnetic energy to propel a space distortion force generated in the space itself. It is to provide a space-driven propulsion device that uses force.

[0010]

In order to achieve the above object, the propulsion device for a flying vehicle of the present invention has the following configuration. That is, the propulsion device for a flying vehicle according to the first aspect of the invention is a magnetic energy that generates a strong magnetic field for changing the curvature components of the inside of a flying vehicle (aircraft, manned rocket, spacecraft, etc.) and the space around the flying vehicle. Generating means; controlling the generation mode of the strong magnetic field by the magnetic energy generating means to locally control the change of the curvature component of the space in a quasi-antisymmetric manner, and to generate a spatial distortion force equivalent to gravity generated in the space. And a magnetic control means for setting the propulsive force of the flying object.

A projectile propelling apparatus according to a second aspect of the present invention is the projectile propelling apparatus according to the first aspect of the present invention; wherein the magnetic energy generating means is a spherical body made of a superconducting material which is a main superconducting magnet for generating a spherical magnetic field. The magnetic control means arranges an auxiliary superconducting magnet that generates a magnetic field of opposite polarity in a hemispherical magnetic field on one side of the main superconducting magnet, and a repetition frequency of exciting current pulses of both superconducting magnets. To control change;
It is characterized by that.

A projectile propelling apparatus according to a third aspect of the present invention is the projectile propelling apparatus according to the first aspect of the present invention; the magnetic energy generating means is a liquid metal storage container for storing a liquid metal that is a highly conductive fluid; A spherical blanket which is a container for generating a strong magnetic field; a liquid metal from the liquid metal storage container as a fluid as it is, or as a spray-like fluid particle
A nozzle for injecting into the blanket; a pair of superconducting magnets arranged to face opposite wall portions of the blanket to generate an initial magnetic field in the blanket;
A pair of laser light sources, which are arranged opposite to the blanket wall portions on both sides orthogonal to the arrangement direction of the pair of superconducting magnets, and irradiate pulsed laser light on fluid particles or fluids with frozen magnetic flux; Fluid particles or
An exhaust pump for returning a fluid to the liquid metal storage container; and the magnetic control means, wherein the magnetic control means controls the excitation current to the pair of superconducting magnets, the asymmetric control of the pair of laser light sources, and the fluid particles or Controlling the process from fluid injection to evacuation at high speed;

[0013]

Next, the operation of the projectile propelling apparatus of the present invention constructed as described above will be described. Propulsion of the present invention, conventional jet engine, rather than by reaction thrust (momentum thrust) by gas fluid ejection such as rocket engines, the pressure difference type by field distortion of the space by the pressure differential thrust to thrust It is a space-driven propulsion system. The outline is as follows.

In terms of continuum mechanics, the field-filling body is affected by the field quantity gradient. For example, sized particles move under the net pressure of a hydrostatic pressure gradient. As a field quantity, this quantity (hydrostatic pressure) is a function of location, and this pressure gradient is an important driving force. An object in a pressure gradient field moves under a net pressure difference. An object in the field of zero pressure remains stationary and does not move. It is assumed that this object generates a locally antisymmetric unidirectional pressure field around the object. In this state, the action of the pressure field on the space of the object and the action of the generated pressure field on the object are in equilibrium, so that there is pressure from the field, but the object cannot move.

Next, the action of pressure field generation on the space of the object is interrupted. Even if this action is instantaneously removed, the space does not instantaneously return to the original state of natural pressure 0, but it takes a finite time to return to pressure 0. That is, the space has a finite strain rate. In this finite time domain, the object and space fields are independent, the object is in the pressure field,
It moves under the pressure of the field. This pressure is equivalent to the net pressure difference in the pressure gradient. ON-O of this pressure field generation action
Continuous thrust is obtained by repeating the FF process at high speed. Energetically, the surrounding space is locally deformed by the pressure field generating action of the object, and the strain energy stored in the space in the form of strain by this displacement action is released by the momentary interruption of the pressure field generating action. , Strain energy of the space excluding some energy loss will be given to the object as kinetic energy when released. Here, the field pressure in space is a surface force generated from the curvature of space generated by a strong magnetic field.

This propulsion principle is derived from a new concept of space and a theory of mechanical structure of space determined from geometrical properties of space. That is, the “distortion” used here means a distortion defined on continuum mechanics, but the distortion of space is generated by the curvature of the space, and the curvature of the space is generated by the mass of the object or the magnetic field. Then, the distortion field of the space due to the object mass is the gravitational field. The magnetic field becomes equivalent to the gravitational field through the medium of curvature (distortion) of space.

Therefore, in the present invention, the generation mode of the strong magnetic field generated by the magnetic energy generation means is controlled by the magnetic control means so that the dynamic curvature change of the space area including the flying object becomes local, and the space itself is controlled. The propulsive force is the spatial distortion force (specifically, the force obtained from the field of the distorted space in the transition process in which the curved space returns to a flat space with zero curvature). This will be described below from another viewpoint. Space
When bent, an acceleration field is formed in the curved space area.
Mass bodies in the field of acceleration are estimated by Newton's second law
Move under the force.

Therefore, this propulsion system is a kind of pressure difference propulsion system utilizing the proximity action (the concept that a direct action is received from the field) due to the strain of the space field, or the force generated by the strain of the space. Is equivalent to gravity and can be called a gravity field propulsion system . Since the thrust force is a volume force that permeates the entire space area including the flying object (a force that is uniformly distributed inside the volume element and is proportional to the mass of the volume element, and gravity and inertial force are also volume forces), it does not receive inertial force. In addition, it has excellent characteristics as a propulsion system of a flying object, such as theoretically achieving a quasi-light speed in a short time. Hereinafter, a mechanical structure of space (space distortion theory), a propulsion operation principle, and the like necessary for understanding the background of the present invention will be described.

Space Distortion Theory I. Basic Concept of Space (1) Space is an infinite continuum whose structure is determined by the framework of Riemannian geometry. There is only one undistorted natural state (flat space) in the space, and when all the external physical effects causing the distortion are removed, the space always returns to the undistorted natural state. Adjacent points in space remain as adjacent points under any physical action, and the change is continuous, and the basic condition that it is a continuum after the change is satisfied. It is a continuum in the sense that it satisfies this hypothesis. The space as a continuum is Riemann space, and its structure follows Riemannian geometry.

(2) Bending of space is a purely geometric quantity. In order to relate this geometric quantity to the actual force, the concept of strain in continuum mechanics is important. The strain field is the point of contact between the geometric quantity and the actual mechanics.

(3) Consider the local change in the geometrical structure of the space as the distortion state of the space. The change in the geometrical structure is a change in the curvature component, which indicates a transition from a flat space (Minkowski space) with a curvature component 0 to a fully curved space (Riemann space) with a curvature component. The fact that the space is bent and the space is distorted are essentially the same.

(4) The distortion of the space represents a kind of deformation of the space, and the material points filling the space are affected by the deformation of the space. An important analytical technique that associates the concept of continuum mechanics as a deformation with the concept of Riemannian geometry is vector translation. If the curvature is not 0, the result of translation of the vector varies depending on the path along the way due to the bending of the space, and the vector does not return to the initial value even if the vector goes around the closed curve on the curved surface. When the curvature is 0, this phenomenon does not occur.

(5) The material occupies an area in space in a continuous manner. Here, space and matter must be clearly distinguished. The substance fills the space and moves to occupy a region of the space. That is, the substance can move in the space, and moves in the space to fill the space.

[0024] (6) the continuity of space for one holding the moving speed of the material point of filling the space does not exceed the strain rate of space.

II. What is Riemannian geometry? Riemannian geometry is a geometry that deals with curved spaces. That is, in this paper, we focus on the curvature of the space, focusing on the four-dimensional Riemann space as a curved space. The target physical space is three spatial coordinate axes (x = x ¹ , y = x
^It is a four-dimensional Riemann space with ² , z = x ³ ) and one axis of time coordinates (w = ct = x ⁰ ). This is x ⁱ (i = 0, 1, 2,
Notated as 3).

The square of the infinitesimal distance ds between the point x ⁱ in the four-dimensional Riemann space and the two points at the adjacent point x ⁱ + dx ⁱ is given by Equation 1. g _ij is called a metric tensor, is a quantity that defines all geometric properties of space, and is generally a function of location. The starting point of Riemannian geometry is a metric tensor g _ij that defines an infinitesimal line element between two points. From the combination of g _ij , the Riemannian connection coefficient (Equation 2),
Furthermore, the Riemann curvature tensor (Formula 3) is defined, and the geometry of the entire space is determined.

[0027]

[Equation 1]

[0028]

[Equation 2]

[0029]

[Equation 3]

Next, the properties of the Riemann space are as follows. (1) In a flat (non-bending) space, all components of the Riemann curvature tensor are 0. In a curved space, the component of the Riemann curvature tensor is not zero. 1 is not 0
If so, the space is essentially curved.

(2) The necessary and sufficient condition for the space to be flat is that all 20 independent components of the Riemann curvature tensor are zero.

(3) In a flat space, the metric tensor has a constant value. In a curved space, the metric tensor is a function of location. That is, the metric tensor deviates from a flat value (Minkowski metric).

III. Basic structural formula of space ds is a line element between any two points in the spatial region I before structural deformation.
= G _i dx ⁱ , the infinitesimal distance is ds ² = g _ij d
x ⁱ dx ^j (left in FIG. 1). Then, in the spatial region II after the structural deformation of the space due to an external physical action (effect of the presence of matter or electromagnetic energy), the line element connecting the same two points in the same spatial region is newly changed and , Ds ′ = g _i ′ dx ⁱ ′, and the infinitesimal distance is ds ′ ² = g _ij ′ dx ⁱ dx ^j (right in FIG. 1). g _i ′ is the transformed and transferred basis vector g _i , and g _ij ′ is the metric tensor of the transformed coordinate system.

Since the degree of deformation can be expressed as a change in the distance between any two points, the following equation 4 is obtained.

[0035]

[Equation 4]

That is, the degree of geometrical structural deformation of space is described by the amount of change r _ij = g _ij ′ −g _ij of the metric tensor. This state of deformation can be expressed using the displacement vector u extended from the position before the deformation to the position occupied by the same coordinate point after the deformation for each point (Equations 5 and 6).

[0037]

[Equation 5]

[0038]

[Equation 6]

Using the above equation, the squared d of the transformed line element
When making a s' ^2, the equation (7).

[0040]

[Equation 7]

In Expression 7, the second-order minute term u ^k : _i u
_k : _j can be sufficiently ignored if the displacement is small. Here, the symbol ":" indicates a covariant derivative.

The covariant derivative is expressed by the equation (8) and differs from the ordinary derivative A _i , _{j by} the quantity of the second term. In a flat space, Riemann connection coefficient Γ ^r _ij = 0, so A _i : _j = A
_i , _j , that is, the covariant derivative of the first-order tensor (vector) A _i and the ordinary derivative match. In a curved space, it is usually necessary to correct the derivative, which is expressed as a covariant derivative.
Therefore, when the derivative of the field quantity is included, it is general to express it as a covariant derivative.

[0043]

[Equation 8]

Since the actual physical space can be treated as a minute displacement from the trial calculation of the order of strain, the second-order minute term can be ignored, and therefore, Equation 9 is obtained.

[0045]

[Equation 9]

On the other hand, as the concept of strain in continuum mechanics,
Since the distortion tensor e _ij is given by Expression 10, the relational expression of Expression 11 is obtained.

[0047]

[Equation 10]

[0048]

[Equation 11]

[Mathematical formula-see original document] Equation 11 is an equation showing a certain kind of deformation in the geometrical structure of space by the concept of distortion. It is shown that a strain field e _ij is generated when the metric tensor shifts from g _ij to g _ij ′ due to the presence of a substance or the like.

IV. Fundamental Equation of Space An important analysis method that associates the concept of continuum mechanics as a deformation with the concept of Riemannian geometry is the concept of vector translation. Mathematical Expression 12 is obtained by expanding the concept of vector translation on Riemann space.

[0051]

[Equation 12]

In Equation 12,

[0053]

[Outer 1]

Is the Riemann curvature tensor

[0055]

[Outside 2]

It is an antisymmetric tensor due to the property of, and becomes a rotation tensor indicating the rotation of the displacement field. When the space is curved, rotation of displacement (field) occurs in the region of the space.

Now, the above-mentioned rotation tensor and strain tensor are expressed in continuum mechanics.

[0058]

[Outside 3]

Satisfies the following differential equation (equation 13) regarding the displacement gradient in the direction perpendicular to the plane of rotation. This equation holds because the order of differentiation is reversible in a flat space.

[0060]

[Equation 13]

Then, in order to extend the differential equation of Equation 13 to the curved Riemann space, the equation needs to be modified into covariance, which is possible under the condition that Equation 14 holds, and A covariant differential equation is obtained.

[0062]

[Equation 14]

[0063]

[Equation 15]

[Mathematical formula-see original document] Next, this equation 15 shows that the displacement gradient of the rotation tensor corresponds to the difference of the displacement gradient of the strain tensor.

[0065]

[Outside 4]

[Formula 16] is obtained by formally multiplying. Incidentally, by using continuum mechanics on the stress (field) tensor sigma ^ij and distortion (field) relationship between the tensor e _m1 and (Equation 18), also the fourth order tensor were treated as constants for covariant derivative . As mentioned above, the symbol ":" indicates a covariant derivative.

[0067]

[Equation 16]

[0068]

[Equation 17]

[0069]

[Equation 18]

On the other hand, the volume force X ⁱ and the stress (field) tensor e ^ij are given by Equation 19 depending on the equilibrium condition in the continuum.

[0071]

[Formula 19]

Therefore, the equation 17 is the change amount ΔX ^{i of the} volume force.
Therefore, Equation 20 is obtained from Equations 16 and 17.

[0073]

[Equation 20]

Equation 20 shows that the spatial distortion force is generated by the gradient of the Riemann curvature tensor showing the bending of the space. The spatial distortion force generated here is a volume force that permeates the space and an object filling the space.

V. Structure of Space Curvature The curvature of space is determined by the Riemann curvature tensor. The Riemann curvature tensor is given by Equations 21 and 22.

[0076]

[Equation 21]

[0077]

[Equation 22]

The Riemann curvature tensor is a metric tensor.

[0079]

[Outside 5]

The structure of the space is determined by this metric tensor, since Then, the solution of this metric tensor is determined by the gravity field equation.

Further, it is a scalar curvature R and a rich tensor.

[0082]

[Outside 6]

And Riemann curvature tensor have the following relationship (Equation 23).

[0084]

[Equation 23]

Represents a material energy tensor

[0086]

[Outside 7]

When the above is applied to the gravitational field equation, the equation 24 is obtained. When this is expanded, the equation 25 is finally obtained.

[0088]

[Equation 24]

[0089]

[Equation 25]

On the other hand, the material energy tensor is given by
Given in.

[0091]

[Equation 26]

[Mathematical formula-see original document] where ρ is the rest mass density,

[0093]

[Outside 8]

Together with

[0095]

[Outside 9]

Indicates a four- way speed.

[0097] Now, the speed of the material is assumed to sufficiently small compared to the speed of light c, 4-way velocity is given by Equation 27. Therefore, the maximum component of matter energy tensor is μ =
Since ν = 0, Y ⁰⁰ is given by Equation 28.

[0098]

[Equation 27]

[0099]

[Equation 28]

Therefore, by substituting the equation 28 into the equation 25, the material energy tensor, that is, the maximum component R ^{00 of the} curvature due to the static mass density is obtained (the equation 29).

[0101]

[Equation 29]

Equation 29 shows that the static mass density ρ controls the curvature of space. The magnetic field B also controls the curvature of the space as described later. In other words, the mass density and magnetic field generate the space curvature.

Now, considering a space that can be approximated by a static and spherically symmetric Schwarzschild spacetime, the scalar curvature R is given by Equation 30.

[0104]

[Equation 30]

The Riemann curvature tensor on the Riemann space and the Gaussian curvature K on the two-dimensional subspace embedded in the Riemann space have the relationship of Expression 31. Further, the scalar curvature R and the Gaussian curvature K of Expression 32 I have a relationship. Therefore,
From Expression 31, Expression 33 is obtained for the two-dimensional Riemann space.

[0106]

[Equation 31]

[0107]

[Equation 32]

[0108]

[Expression 33]

VI. Curvature control of space by magnetic field The electromagnetic energy tensor M ^ij is applied to the gravitational field equation. In this case, the metric tensor g _ij is given by Equation 34.

[0110]

[Equation 34]

Equation 34 is an equation for determining the structure of the space due to electromagnetic energy. By multiplying Equation 34 by g _ij and transforming it, Equation 35 is obtained. From both equations, the following equation (Equation 36) is obtained. can get.

[0112]

[Equation 35]

[0113]

[Equation 36]

Antisymmetric tensor f _ij indicating the magnitude of electromagnetic field
By using the electromagnetic energy tensor M
^{Since ij} is given by Expressions 37 and 38, the value of M is obtained as follows (Expression 39).

[0115]

[Equation 37]

[0116]

[Equation 38]

[0117]

[Formula 39]

By substituting M = 0 into Equation 36,
Equation 40 is obtained.

[0119]

[Formula 40]

The rich tensor R ^ij has 10 independent components, but the main component is i = j = 0, that is, R ⁰⁰ . Therefore, Equation 41 is obtained from Equation 40.

[0121]

[Formula 41]

On the other hand, the antisymmetric tensor f _ij = -f _ji is given by the electric field E and magnetic field B in relation to Maxwell's electromagnetic equation (Equation 42).

[0123]

[Equation 42]

By substituting the equation 42 into the equations 37 and 38, the equation 43 is obtained, and finally the equation 44 is obtained. In addition,
In both equations, μ ₀ is 4π × 10 ⁻⁷ (H / m), ε ₀ is 1 / 36π × 10 ⁻⁹ (F / m), and c is 3 × 10 ⁸ (m / m).
s), B is a magnetic field (Tesla), and G is 6.672 × 10 ^-11 (N
M ² / kg ² ), R ⁰⁰ is the curvature component (1 / m ² ) of the space.

[0125]

[Equation 43]

[0126]

[Equation 44]

Equation 44 shows that the main curvature component of space is controlled by the magnetic field B. It is possible to control by the electric field E, but if E and B of the same size are 1 /
The value of 2 · ε ₀ E ² is about 1 compared with the value of 1 / 2μ ₀ · B ^2.
Since it is as small as 7 digits, the contribution of the electric field E to the curvature can be sufficiently ignored as compared with the magnetic field B.

On the other hand , the main curvature component by the material energy tensor Y ^ij is given by equation 45.

[0129]

[Equation 45]

Since the curvature component R ⁰⁰ of the space is not related to the factor of the material energy or the electromagnetic energy tensor as its generation source, the expression 46 and the expression 47 are derived.

[0131]

[Equation 46]

[0132]

[Equation 47]

Since B ² / 2μ ₀ = W represents the energy density (J / m ³ ) of the magnetic field, it has the following relationship with the rest mass density ρ (kg / m ³ ) (Formula 48). Formula 48 guarantees the relational expression of mass and energy, E = mc ² .

[0134]

[Equation 48]

VII. Field pressure due to space curvature (surface force)
Generation Since the basic structure of the three-dimensional space is determined by the quadric surface structure, the Gaussian curvature K in the two-dimensional Riemann space gives a practical concept (Equation 49).

[0136]

[Equation 49]

By applying the film theory to this quadric surface, the following equilibrium conditional expression is obtained (Equation 50).

[0138]

[Equation 50]

In the equation 50,

[0140]

[Outside 10]

Is the film force (linear stress),

[0142]

[Outside 11]

Is the second basic metric of the curved surface, and P ³ is the vertical stress (surface force) on the curved surface.

The second basic metric of a curved surface has the following relationship between the principal curvature of the curved surface and the metric tensor (Equations 51, 5).
2).

[0145]

[Equation 51]

[0146]

[Equation 52]

Therefore, Equations 50 to 53 are obtained.

[0148]

[Equation 53]

Since α and i take a binary value with respect to the quadric surface, the expression 54 is obtained. Note that in Equation 54, K
₍₁₎ , K ₍₂₎ are the principal curvatures of the curved surface, and the principal curvature radius R ₁ ,
It is the reciprocal of R ₂ .

[0150]

[Equation 54]

Since the Gaussian curvature K is given by the equation 55, the equation 56 is obtained on the assumption that the film force N ¹ ₁ = N ² ₂ = N.

[0152]

[Equation 55]

[0153]

[Equation 56]

That is, the film force and the principal curvature on the curved surface generate a vertical stress P ³ (N / m ³ ) as a surface force on the curved surface,
The direction is toward the inside of the curved surface.

Now, let us consider a curved surface of a thin layer in a spherical mold space in which both the principal curvature radii R ₁ and R ₂ are equal to the radius R. Since the Gaussian curvature K is expressed by the equations 49 and 55, the equation 57 is obtained.
Substituting 1 / R = (R ^00/2 ) ^1/2 into the equation 56 gives the equation 58 and the equation 59 is obtained.

[0156]

[Equation 57]

[0157]

[Equation 58]

[0158]

[Equation 59]

Since the film force N in the space as the linear stress is considered to be a unique constant value under a constant condition, the expression 59
Therefore, the curvature of R ⁰⁰ generates a vertical stress P ³ as a surface force of the space inward of the curved surface. The vertical stress P ^{3 in} the inner direction of the curved surface is the pressure of the field, that is, the accumulation of a large number of curved surfaces in the area of the space forms a unidirectional pressure field.
Here, the surface force of the curved surface of the thin layer of space = the vertical pressure in the inner direction of the curved surface = the pressure of the field = −P ³ (N / m ² ) are all synonymous,
It is only the difference in perspective. The surface force field is a kind of force field and gives an acceleration to a substance in a region of space, so that a field of acceleration is generated. From the above, the curvature of the space (Curvature) is the surface force on the space itself.
To generate a unidirectional acceleration field in the spatial region.

VIII. Curvature of space and acceleration field An inward surface force is generated in the curved thin film layer itself due to the curvature of space, and an acceleration field is formed in a certain spatial region by the integration of these thin film layers. The strength α of the acceleration field and the main curvature component R ⁰⁰ of the space caused by the geometrical structure of this space are such that the curvature of the space is relatively small and the distortion field is weak, and this field is temporal. In the static case, the equations 60 and 61 are given by comparison with Newtonian dynamics.

[0161]

[Equation 60]

[0162]

[Equation 61]

[0163] Here, h ₀₀ represents the deviation between the Minkowski metric eta ₀₀ = -1 flat space and the metric tensor g ₀₀ of curved space, Equation 62, a relationship of the 63.

[0164]

[Equation 62]

[0165]

[Equation 63]

From Equations 62 and 63, the relationship between the curvature of the space and the acceleration field is Equations 64 and 65.

[0167]

[Equation 64]

[0168]

[Equation 65]

Further, from the equations 60 and 61, the equation 66 is obtained.

[0170]

[Equation 66]

Equation 66 is a distortion of space e ₀₀ (= 1/2 ·
It is shown that the distance gradient of h ₀₀ ) produces an acceleration field α. Further, it can be seen that the Riemann connection coefficient Γ ⁱ _{00, which} is a geometric quantity, corresponds to the physical quantity, which is the distortion gradient, e ₀₀ : _i .

[0172] space in static spherically symmetric Schwarzschild spacetime components gamma ⁱ ₀₀ is a Riemannian connection coefficient is not 0, the component of the i = 3 toward the radial direction of the sphere, that is, only gamma ³ ₀₀ .. Therefore, R ⁰⁰ is given by Equation 67, and the acceleration α ³ = α is given by Equation 68.

[0173]

[Equation 67]

[0174]

[Equation 68]

Equation 68 shows that the acceleration α received by an object in the field of acceleration is proportional to the distance integral of the curvature R ⁰⁰ of the space.

In Newtonian mechanics, the acceleration α is given by the potential Φ: _i . Here, Φ is given by Expression 69, and since α = Φ: _i and Expression 60 result in Expression 70, h ₀₀ becomes Expression 71. Therefore, R ⁰⁰ becomes the formula 72.

[0177]

[Equation 69]

[0178]

[Equation 70]

[0179]

[Equation 71]

[0180]

[Equation 72]

On the other hand, the acceleration is obtained by the following equation (equation 73), and the value on the surface of the earth is obtained by substituting the radius and mass of the earth (equation 74).

[0182]

[Equation 73]

[0183]

[Equation 74]

The relational expression between the magnetic field and the curvature (Formula 75)
Therefore, the strength of the magnetic field that generates the curvature of space 3.42 × 10 ^-23 is 20 million Tesla.

[0185]

[Equation 75]

Next, the relationship between the curvature of space and the acceleration field will be examined. It has already been mentioned that the surface force of the spatial field generated by the curvature R ⁰⁰ of the spatial space is given by P ³ = N · (2R ⁰⁰ ) ^1/2 . The curvature R ⁰⁰ of the space on the surface of the earth is
Given by 3.42 × 10 ^-23 , the object in the space field at that point receives 1G of gravitational acceleration from the field. The value of curvature is extremely small, but it is large enough to cause 1G acceleration on the ground surface. Strictly speaking, although given the acceleration of the object with a gradient of surface forces, true essential for generating the acceleration field by considering a sufficiently small local area of current space
Corresponding to acceleration is approximately obtained by the surface force P ³ which is a factor .

The curvature R ⁰⁰ of the space which produces the surface force P ³ which gives the field of acceleration of 1 G is brought about by the mass density of the earth, but the curvature of the space is also brought about by the magnetic field as described above. Curvature, as a property of space, must have the same result independent of its origin. Therefore, 1G = P ³ = N ・ (2 * 3.42 * 10 ^-23 ) ^1/2 = N ・
From (2 * 8.2 * 10 ^-38・ B ² ) ^1/2 , B = 20M Tesla
Becomes

[0188] Now, if, when the size of the earth mass 100 times that is the density in intact is 100 times, the curvature of the space on the surface in the R ⁰⁰ = 3.42 * 10 ^-21, the corresponding acceleration field Has a strength of 100 G, and the corresponding magnetic field strength is 200 M Tesla using the same method as above. The same idea gives the following table.

[0189]

[Table 1]

Here, it should be noted that
It means that the value of the curvature R ^{00 and} the value of the acceleration α do not have a one-to-one correspondence. As can be seen from Expression 65, the curvature, that is, how much the space is curved does not correspond to the acceleration value itself, but corresponds to the degree of change in acceleration, that is, the gradient of the acceleration field.

Alternatively, from Equation 73, the acceleration corresponds to the integral of the distance of curvature, that is, the area range (Volume) of the curved space.

The comparison here is a comparison between the spherical surface of the substance called the earth and the spherical surface when the magnetic field is confined in a spherical shell. It should be noted that the strain potential as a body distribution density function satisfies the Laplace equation at the outer point of the surface of the sphere, that is, in free space, and therefore decays as a function of the distance r. The values in the table give a rough guide.

IX. Gravity and inertial force Both the magnitude of gravity and the inertial force are proportional to the mass of the volume element, permeate into each part of the body from the outside, are evenly distributed inside, and act uniformly on all internal material points. Is the force to do, and both have the property of volumetric force. Inertial force as pseudogravity is equivalent to gravity, and locally canceling gravity is a well-known fact as an equivalence principle. It has already been experienced because it is possible to temporarily achieve weightlessness by turning flight of an aircraft.

In order for all the material points in this volume element to equally act and move, the existence of a gradient of surface force (also called area force), that is, a kind of pressure difference gradient, is essential in this region. That is, in order to move not only the outer shell of the volume element itself but also the volume element's storage evenly, a surface force difference of ΔP is required as a driving force within the volume element (see FIG. 2). .. This mechanism creates an acceleration field.

If the space is assumed to be a continuum for gravity and inertial force, both strain gradients are generated, and although detailed formulas are omitted, the above-mentioned strain gradients generate the above-described surface force distance gradients. Therefore, a volume force that acts uniformly on all material points is generated, and the mechanism is exactly the same.

The essential difference between gravity and inertial force is that gravity has a curvature R ^{00 of} space, whereas inertial force does not have a curvature of space, that is, curvature R ⁰⁰ = 0. In the case of inertial force, since the curvature R ⁰⁰ = 0, the acceleration α is constant regardless of the location (Formula 76).

[0197]

[Equation 76]

However, in the case of gravity, the curvature of the space is a function of the place and is given by Expression 77. Therefore, the acceleration α is a function of the place and is not constant. In other words, with gravity, the value of acceleration changes with location. To be exact, there is a distance gradient, and the degree of change in this acceleration corresponds to the curvature, that is, how much the space is curved.

[0199]

[Equation 77]

Gravity and inertial force are discriminated by the presence or absence of curvature, but both the strain gradient due to the bending of the space and the line strain gradient of the space due to the acceleration motion of the object occur, and the surface force gradient is generated. It has the property of volumetric force.

Principle of Propulsion Operation To summarize the above description, bending of the space causes distortion of the space. The distortion force of the space penetrates and acts on the space and the object filling the space as a field. Such a space bend is generated not only by the mass of the object but also by the magnetic field. That is, the main curvature component R ⁰⁰ of the space can be controlled by the magnetic field (Formula 78). The curvature R ⁰⁰ of the space is a unidirectional pressure field in the space area including the object as the pressure of the space field.
Generate P ³ (Equation 79) , or the curvature of space is
An acceleration field is formed in the defined spatial area (Equation 68).
An object in a unidirectional pressure field moves by receiving this pressure from the field , or an object of mass m in the field of acceleration α
Moves under the thrust of f = mα from this field. This pressure is equivalent to the net pressure difference experienced by an object in the pressure gradient field. This gives the driving principle of the invention.

[0202]

[Equation 78]

[0203]

[Equation 79]

That is, a strong magnetic field causes a bend in a space area near the arrangement area (propulsion section) of the magnetic energy generating means mounted on an object (flying body). However, since the action of changing the curvature of the space and the action of the distortion of the space are balanced by the static magnetic field, there is no propulsion (movement) of the flying object even if thrust is generated. Therefore, in order to propel the flying object, it is necessary to unilaterally break the equilibrium state between the action of the magnetic field on the space and the inverse action from the space, and for that purpose, the magnetic control means is mounted. At this time, the action on the space is performed in a quasi-static process while slowly maintaining the equilibrium state, and the inverse action from the space is instantaneously performed. It is important to control the rate of energy release. It is like a bow and arrow, and is gradually stored as strain energy of the elastic body, and is close to giving momentary energy to the arrow. Therefore, the reverse thrust cannot be generated when the magnetic field is generated.

The magnetic control means controls the generation mode so that the strong magnetic field generated by the magnetic energy generation means changes in a pulse shape or rotates the magnetic field (30 GHz), and the movement of the curvature component of the space is controlled. It produces a dynamic change and obtains continuous thrust from the space field to drive it.

The space has a finite strain velocity (light velocity) as a continuum, and it takes a finite time for the distorted (bent) space to return to a flat space even if the magnetic field is interrupted. .. During the transition process to return to a flat space, the projectile independently exists in the curved space field and can be propelled by the action from this space field.

That is, since the equilibrium state is broken by instantaneously interrupting the action of bending the space, during the minute time of the transition process in which the bent space returns to a flat space without bending,
The projectile is independent of the curved space field, and the projectile can be propelled by the adverse effect of the space field.

[0208] Generally, it is not possible to propel while dragging the place by the place generated by itself. In other words, unless the propellant and the place are independent, it cannot be promoted by the place. This is because the action on the field and the reaction from the field are in equilibrium. At this time, it is important in principle to delay the reaction from the action in time.

Characteristics of this projectile (1) Since the thrust is a volume force, all the material points including the projectile (spacecraft) and the occupants inside the projectile (spacecraft) receive the same force and are accelerated, so There is no action of force.

(2) Navigation such as sudden start, sudden stop, right-angled turn and zigzag turn from the stationary state in the air is possible.

(3) Magnetic field energy acting on space and
Since the power source is built into the spacecraft, it can be used for both planetary atmosphere and space navigation.

(4) The propulsion acceleration can be freely changed from several μG to 100 G by controlling the pulse magnetic field. In other words, the navigation is stable (air stop-low speed-high speed is arbitrary).

(5) Since the thrust is proportional to the mass increase due to the speed increase, the propulsion acceleration is always constant. In addition, since the propulsion operation time is not limited, the final arrival speed of the flying object (spacecraft) is the quasi-light speed.

(6) Since it is not an internal combustion engine, noise (propeller sound, gas injection sound) and injection gas are not generated. Also,
Since it is not equipped with explosive fuel, it is highly safe.

(7) Since thrust acts on the entire space area including the flying object (spacecraft), the flying object (spacecraft) is present in the atmosphere.
Similarly, the air on the outer surface is accelerated and moves, and the occurrence of aerodynamic heating can be reduced. In other words, it only causes friction between air molecules, and the flying object (spacecraft) can move in the atmosphere at high speed (several kilometers per second to several tens of kilometers per second). However, it is expected that the highly heat-ionized air (plasma) will envelop the entire projectile (spacecraft).

(8) Regarding the shape of the flying object (spacecraft), it can be said that a sphere or an ellipsoid has the most excellent functional efficiency in view of the principle of operation and omnidirectionality.

(9) Since the space area around the flying object (spacecraft) is locally curved, the shape of the flying object (spacecraft) changes due to the gravitational lens effect, or the space between the observer on the ground and Depending on the position or distance and the azimuth angle, there may be a blind spot that cannot be seen at all. (10) When the spacecraft propulsion acceleration is 100G and it is required to reach Mars
It takes about 11 hours, and the period required for manned planetary exploration is
Drastically decrease. (11) By controlling the timing to turn off the magnetic field,
It is possible to suck up objects on the lower part of the airship and to release them.

[0218]

Embodiments of the present invention will be described below with reference to the drawings. 3A and 3B show the appearance of a flying object according to an embodiment of the present invention, FIG. 3A is a schematic top sectional view, and FIG. 3B is a schematic side sectional view.

The flying vehicle 1 according to this embodiment is made of an ellipsoidal shape, and propulsion engines (21 to 26) are provided at four outer peripheral positions which divide the outer periphery of the disk into four equal parts and at the central position of the upper and lower surfaces of the disk. There is.

Each of the propulsion engines (21 to 26) is constructed by associating the magnetic energy generating means with the magnetic control means for controlling the magnetic energy generating means in a one-to-one correspondence. Note that one magnetic control unit may be provided as a whole, and all magnetic energy generation units may be collectively controlled.

The magnetic energy generating means generates a strong magnetic field to increase the value of the curvature component of the space around the flying object 1 from 0 or a certain value to a certain value, and as will be described later, acceleration as a space distortion force. To generate a field. The magnetic control means
The change of the curvature component of the space caused by the strong magnetic energy is made quasi-antisymmetric locally, and at the same time, the magnetic field is changed in a pulse shape to obtain the propulsive force, or the rotation of the magnetic field causes the change of the space. The magnetic energy generating means is controlled so that the curvature component dynamically changes.

FIG. 4 shows a state in which the propulsion engine 24 of FIG. 3 (B) is operated. The projectile 1 receives an external force (pressure difference) P-P ' from an asymmetric strain field in space and propels it in the right direction (direction P') in the drawing. The same applies to other propulsion engines, and the propulsive forces in the vertical direction and in the directions orthogonal to each other in the horizontal plane are obtained, and movement of the propulsion engines in arbitrary directions can be controlled by combining these.

For example, in the flying body shown in FIG.
If the engine is shaped as shown in FIG. 5, the four propulsion engines cause sudden start and stop in any direction from a stationary state in the air as shown in FIG. 6 (FIG. 6 (A)). , Horizontal navigation and vertical ascent (descent) combined navigation (Fig. 6
(B)), zigzag navigation (FIG. 6 (C)), and other arbitrary navigation that cannot be obtained by the conventional propulsion method.

Next, although the propulsion operation principle has been described above, in order to make it easier to understand, the practical propulsion concept will be explained first, and then the arrangement of the propulsion engine and the motion of the flying vehicle (spacecraft) in this order. The structural model of the propulsion engine that generates the property, propulsion efficiency, and quasi-antisymmetric space is described.

Conceptual Description of Propulsion Principle For example, an object in the space around the earth moves (falls) toward the center of the earth. The direct cause of the movement of the object is the action due to the distortion field due to the bending of the space around the earth, not the action of the earth itself.
However, the existence of the earth's mass (density) bends the space, so it is an indirect cause for the movement of objects.

When the object is directed toward the center of the earth, a strain field gradient is generated in the direction of the curvature of the space (perpendicular to the curved surface) generated by the mass (density) of the earth, which coincides with the direction of the center of the earth. (Fig. 7). It should be noted that the curved space and the object are independent and have no interaction.

Now, as a hypothetical experiment, it is assumed that the earth does not exist and only the space bend exists in the same region as the above in outer space. Objects in the turn of space will move in exactly the same way (Fig. 8). The curved space and the object are independent without any interaction.

This means that even if the sun disappears instantly on the earth revolving around the sun, its effect will reach the earth after 8 minutes and 32 seconds. Is the same interpretation as the fact that the sun still revolves around the sun.

The principle of this propulsion is that an object (spacecraft) in outer space artificially creates the above-mentioned unidirectional bending of space around the object and instantaneously cuts off the creating action. , To create a state of bending equivalent to the above. However, the state immediately after the generation action is turned off is a transition state in which the curved space returns to a flat space, and the curved space and the object (spacecraft) are independent in this process, and there is no interaction ( (Figure 9).

The acceleration α generated in the curved space region is given by the following formula 80 where R ⁰⁰ is the curvature, c is the light velocity, and r is the integration constant indicating the curved region.

[0231]

[Equation 80]

If the curvature of the space is uniform (constant value) in the area (FIG. 9), the acceleration α is given by equation 81 with the area length being s. Then, the curvature of the space is generated by the mass density ρ or the magnetic field B (Formula 82). In other words, the mass field or the magnetic field creates an acceleration field in the spatial region.

[0233]

[Equation 81]

[0234]

[Equation 82]

Disappearance of an object is impossible unless it is established as a virtual experiment or is actually an explosion. However, the equivalent of the disappearance of an object can be easily controlled by OFF control in a magnetic field.

In order to propel a spacecraft, a distorted surface of space as shown in FIG. 10 is ideal. That is, the region A ′ is a flat space having a curvature R ⁰⁰ = 0, and the region A is a space having an antisymmetric curvature such as a curved space (a distorted space) having a curvature R ⁰⁰ ≠ 0. .. The magnitude of the acceleration field generated in the curved space area A, that is, the acceleration α
Assuming that R ⁰⁰ is uniform, G is the universal gravitational constant, μ
It is as described above that ₀ is given as the magnetic permeability of the vacuum by Expression 83, and the field of acceleration is generated in the spatial region by the magnetic field B.

[0237]

[Equation 83]

However, practically, as shown in FIG.
The distorted surface of space is spherically symmetric about the engine of the spaceship.
No effect on the promotion also. Within a finite time when the spacecraft moves under the thrust of the acceleration field in the region A, the distorted surface of the curved space in the region A ′ has already returned to the flat space (R ⁰⁰ = 0 ), so the region A There is no reverse thrust due to the acceleration field of ′.

Time τ when curved space returns to flat space
Is τ = 1 because the strain rate of the space is the light velocity c.
It is constant at / c. Further, since this thrust received from the acceleration field is a volume force equivalent to gravity and is proportional to the mass of the volume element, there is no spacecraft mass body in the area A ′ in the state of FIG. It can be seen that there is no reverse thrust from ′.

Practically, as shown in FIG. 12, a space in which the strained surface of the region A'is weaker than the strained surface of the region A, that is, (the curvature R ⁰⁰ ′ of the space of the region A ' ) <
It may be a space having a quasi-antisymmetric curvature such that (curvature R ⁰⁰ of space of region A). The space having the quasi-antisymmetric curvature is generated by controlling the magnetic field distribution in the engine of the spacecraft.

Assuming that the antisymmetrically distributed magnetic fields in the engine are B and B ′, respectively, the curvature of the space in the region A is given by the formula 84 and the curvature of the space in the region A ′ is given by the formula 85. Therefore, if B ′ = (1/10 to 1/40) × B is controlled,
The curvature R ⁰⁰ ′ of the space of the area A ′ is R ⁰⁰ ′ = (1/100
~1 / 1600) × R ⁰⁰ next, as a numerical order, R ⁰⁰ '"R ⁰⁰ to be able to quasi-anti-symmetric space.

[0242]

[Equation 84]

[0243]

[Equation 85]

Although there is no spacecraft mass body in the area A ', the acceleration α'in the area A'is the mathematical expression 86, and the acceleration α in the area A is the mathematical expression 87. From R ⁰⁰ '<< R ⁰⁰ , Α ′ << α
Then, the spacecraft can propel the quasi-antisymmetric space of FIG.

[0245]

[Equation 86]

[0246]

[Equation 87]

Further, the time τ in which the curved spaces in both the area A and the area A'return to a flat space is the same, and the space curvature during the movement of the spacecraft accelerated in the area A to the area A'is It has already disappeared, and α ′ = 0. The mass of the spacecraft (mass m) is 'no, because the majority is in the area A, with respect to the thrust f _A = m.alpha by acceleration, f _A' region A ≒
Since 0 × α ′ = 0, the reverse thrust by the area A ′ can be treated as a minute amount from the beginning.

Engine Arrangement Structure and Mobility of Spacecraft (Spacecraft) FIG. 13A shows six engines arranged as shown in FIG. 3. With this arrangement structure, movement in all directions is possible. It is possible. Operates front engine for forward, rear engine for reverse, right engine for right, left engine for left, top for ascent The engine is operated and the lower engine is operated for descent, but since the propulsion direction is a vector combination of the propulsion directions of the engine parts, the projectile can move in all directions.

For example, the left-right turn is performed as follows. At an acceleration of 100G ≒ 1km / s ^2, the operation for one second of the front engine, uniform linear motion of the 0 → 1km / s after one second. That
After 1 second operation of the rear engine, 1 km / s after 1 second
→ Stop at 0. And for 1 second of left engine operation
1 second later, 0 → 1km / s, turn left at a right angle (constant speed straight line operation)
Move).

The engine is formed in the sphere,
As shown in FIG. 13 (B), if the type of engine is one sphere connected to two spheres (small sphere and large sphere) to form a bowling pin, the number of engines is Can be reduced. In the figure, the upper small sphere corresponds to the upper engine and the lower large sphere corresponds to the lower engine.

Even if four pin-shaped engines are arranged as shown in FIG. 13C, they can be moved in all directions. Further, even if three of the pin-shaped engines are arranged in a regular triangular shape, they can be moved in all directions by changing the engine control performance.

Structural Model of Propulsion Engine As a function of the engine, it is required to form a unidirectional surface force field as a pressure of the field of the space by giving a curvature to the space. The thin quadric surface of the space in which the surface force is generated is referred to as a distorted surface of the space. The surface force goes to the inside of this strained surface.

The curvature component of the space controlled by the magnetic field B is given by the expression 88. This strong magnetic field is a superconducting magnet confined in the shell of a perfect diamagnetic material (superconducting material) having spherical strength. Caused by. The reason for using the perfect diamagnetic material is to obtain only the curvature of the space without confining the magnetic field in the engine inside and outputting it to the external space. In the space around the engine, a spherical distortion surface is generated as a spherically symmetric field (Fig. 14).

[0254]

[Equation 88]

Since the engine receives the surface force toward its center in a spherical symmetry from the distorted surface of the space, the surface force is balanced and cannot move. However, other substances in the strain field around the engine move toward the center of the engine due to the surface force in the direction of the spherical center.

For propulsion, the engine requires the generation of an antisymmetric unidirectional strain field in the region of space. That is, the curvature R in one half of the space around the engine
⁰⁰ ≠ 0 (curved space), R ⁰⁰ = in the other half area
It is necessary to generate an antisymmetric field of 0 (flat space) by controlling the direction of the magnetic field.

Therefore, the principle structure of the magnetic energy generating means in the propulsion engine is as shown in FIG.
A main superconducting magnet 31 that generates a spherically symmetric magnetic field, and an auxiliary superconducting magnet 3 that is arranged in the hemispherical magnetic field on one side of the main superconducting magnet 31 so that the polarities of the magnetic fields are opposite.
It is composed of 2 and. Since the magnetic field required for propulsion has a value of several tens of billions of tesla, it cannot be realized by the usual magnetic field generating means, so a superconducting magnet is used.

As a result, the antisymmetric unidirectional strain field shown in FIG. 16 is generated. Since the engine receives antisymmetric surface forces, it moves in one direction toward a flat space area with zero curvature. Other substances in the space region (curvature ≠ 0) on one side of the engine also move toward the flat space region having a curvature 0. Therefore, by controlling ON / OFF of the generation of the magnetic field, the flying object (spacecraft) can be propelled.

The magnitude of the magnetic field is B ² = B · B = │
Since it is given by B│2, ^two different magnetic fields B ₁ , B
_{2. If} the synthetic magnetic field is B _T , Equation 89 is obtained. Then, when the two magnetic fields have the same magnitude, Equation 90 is obtained when the directions of the magnetic fields are forward, and Equation 91 is obtained when the directions of the magnetic fields are opposite.

[0260]

[Equation 89]

[0261]

[Equation 90]

[0262]

[Formula 91]

Propulsion Efficiency and Energy Formula Next, the propulsion efficiency of the present propulsion engine will be examined from the viewpoint of energy conversion in order to explain the magnetic control means. The conversion flow is as follows: supplied power energy (P _WE ) → superconducting magnetic field energy (E _MAG ) → space curvature (R ⁰⁰ ) → strain energy stored in space (U _STRAIN ): = engine output energy (E _NG P _WR ) →
Emission of spatial distortion energy → Effective propulsion energy (E _EFP )
+ Reactive propulsion energy (E _LOS ) + Radiant energy (E _RAD ) The efficiencies in each phase are given by equations 92 to 95,
The efficiency η of the entire engine is given by Equation 96.

[0264]

[Equation 92]

[0265]

[Equation 93]

[0266]

[Equation 94]

[0267]

[Formula 95]

[0268]

[Equation 96]

The strain energy U stored in the space
_STRAIN (engine output energy) is given by equation 97, and (effective propulsion energy + reactive propulsion energy + radiation energy) is given by equation 98.

[0270]

[Numerical Expression 97]

[0271]

[Equation 98]

In Expression 98, V ₁ and ρ ₁ are the volume and average density of the flying object, V ₂ and ρ ₂ are the volume and average density of a finite area around the flying object (atmospheric density in the atmosphere), h And ν are Planck's constant and radiant energy frequency. That is, the reactive propulsion energy means an energy loss for similarly accelerating the surrounding atmosphere because the main thrust is a volume force. Further, it is considered that not all spatial distortion energy is converted as propulsion energy, but a part thereof is emitted as radiant energy.

The overall efficiency of the engine is given by the mathematical expression 99 from the viewpoint of power.

[0274]

[Numerical expression 99]

In Expression 99, f is the volume force of the field (N /
m ³ ), V is the operating area (m ³ ), fV = F is the thrust (N), v is the propulsion speed (m / s), ν is the superconducting engine excitation cycle number,
E is the superconducting coil exciting voltage (V), I is the superconducting coil exciting current (A), and τ is the current pulse width (s).

In short, from the formula 99, the propulsion speed can be controlled by changing the engine excitation cycle number ν, and the thrust basically depends on the power EI of the power source and is controlled by changing the exciting current I.

Finally, the magnetic control means is configured to control the repetition frequency of the exciting current pulse. As a result, the magnetic field changes in a pulse shape and a dynamic change in the curvature of the space can be obtained with the ON / OFF of the magnetic field, and the flying space (spacecraft) has a flat curved space when the magnetic field is cut-off. The thrust as an action from the space field can be received in a pulsed manner at the instant of the transition process returning to a normal space and propelled.

Now, a specific example of the magnetic field generating means will be described.
This obtains a strong magnetic field by magnetic flux freezing and laser light implosion (FIG. 17, FIG. 18, FIG. 19).

First, the magnetic flux freezing will be briefly described. Magnetic flux freezing, also called magnetic field freezing, is a phenomenon in which when a highly conductive fluid moves in a magnetic field, magnetic flux (lines of magnetic force) attach to the fluid and try to move together. In principle, when there is relative motion between a highly conductive fluid and a magnetic field, a current is induced by electromagnetic induction, and this current interacts with the magnetic field to cancel the relative motion between the fluid and the magnetic field. As a result, the fluid and the magnetic field move together as if the lines of magnetic force were attached to the fluid. Since the magnetic field is attached (frozen) to the fluid, the lines of magnetic force are dragged and deformed or strengthened by the motion of the fluid.

This phenomenon is proposed as a hypothesis that explains the magnetic field of celestial bodies as a fossil mechanism. In other words, when the magnetic field lines are frozen in the gas when the star is born due to the contraction of the interstellar gas, the magnetic field lines are concentrated as the gas contracts, and the star has a poloidal magnetic field. It is estimated to be about 500 million tesla for a neutron star, which is the same as the observation result.

Now, in FIG. 17, (a) shows a state in which magnetic flux (lines of magnetic force) is frozen in the highly conductive fluid particles,
(B) shows a state in which the fluid particles contract due to the action of an external force or the like, and the lines of magnetic force also contract accordingly, and (c) shows a state in which the fluid particles further contract and become a poloidal type. Since the magnetic flux frozen in the fluid particles also performs the same contraction movement as the fluid particles contract, only the magnetic flux passage area S (m ² ) contracts and decreases while the magnetic flux φ (Wb) is preserved. Therefore, the magnetic flux density, that is, the strength of the magnetic flux B (Tesla) is B = φ / S, and its value increases and the magnetic field is concentrated.

FIG. 18 shows the principle of strong magnetic field concentration.
An initial magnetic field is applied to the sprayed fluid particles of the highly conductive liquid metal or the liquid metal that has been poured as it is, and the magnetic flux is frozen. Then, laser light is irradiated from the four sides to the region of the fluid particles or the liquid metal whose magnetic flux is frozen. Irradiated fluid particles or surface of the liquid metal starts ejection of the heated plasma, fluid particles or liquid gold
The genus is compressed toward the center due to the reaction of the plasma jet.
A so-called implosion effect is achieved, and it plays a role of further increasing the contraction effect of the light pressure by the laser light. Note that an asymmetric distribution of the magnetic field can be obtained by controlling the left and right laser light intensities (for example, the right intensity> the left intensity).
The auxiliary superconducting magnet 32 shown in 5 can be eliminated.

As described above, the fluid particles or the liquid metal rapidly contracts due to the light pressure of the laser beam and the ablation (jetting) pressure generated by the reaction of the high temperature plasma gas, so that the magnetic flux frozen in the fluid particles also contracts. , Magnetic field enrichment is achieved.

The laser light power density S (W / m ² ) is given by S = u · C, where u (Pa: = N / m ² ) is the light pressure and C is the light velocity value. Also, considering the area ratio (1 / r) due to concentration, the laser light power density is S = u · C · (1 /
r).

Since the laser light power density currently in practical use is about 10 ¹⁷ to 10 ¹⁸ (W / cm ² ), assuming that a radius ratio of 1/1000 due to concentration, the area ratio is 1 / r. = 1/10
^{From 6} , S = 10 ¹⁷ (W / cm ² ) = 10 ²¹ (W / m ² ), and the laser light pressure u becomes 10 trillion atmospheric pressure. Due to the light pressure including the implosion effect of the laser light, the magnetic flux frozen good-conducting fluid particles are rapidly contracted and a strong magnetic field is concentrated.

Next, FIG. 19 shows a strong magnetic field generator.
This strong magnetic field generator generates a nozzle 42 for injecting a liquid metal as a highly conductive fluid as a fluid as it is or as a sprayed fluid particle into a blanket 41, and an initial magnetic field (seed magnetic field) in the blanket 41. superconducting mug nets 43 to be, the same 44, the laser light source 45 to provide light pressure and implosion effect fluid particles or liquid metal and flux frozen in the blanket 41, the same 46, the fluid flux freeze is released Exhaust pump 4 for exhausting particles or liquid metal
7 and a liquid metal storage container 48, which is a device that can continuously generate a pulse magnetic field of several hundreds of thousands to several tens of billions of tesla.

In FIG. 19, the initial magnetic field (seed magnetic field) is set to 5
An operation of continuously generating a pulse magnetic field of 500,000 Tesla will be described with 0 Tesla. First, the highly conductive liquid metal is sprayed from the liquid metal storage container 48 by the nozzle 42 as atomized particles.
Alternatively, the liquid metal is directly injected and injected into the blanket 41. After that, the upper and lower superconducting magnets (43, 4,
The initial magnetic field (5
0 tesla). The magnetic field is frozen in the injected fluid particles or liquid metal .

Next, the fluid particles or the liquid metal is irradiated with pulsed laser light from the laser light source (45, 46). The power density of this pulsed laser light is 10 ¹⁸ W / cm ² = 10 ²² (W / m ² ).
Is. At this time, light pressure is ^{10 22/3 * 10 8 =} 3 * 10 13 Pa
It is equivalent to 300 million atmospheric pressure. Then, by a laser beam implosion effect, assuming a radius ratio 1/100, since at Area Ratio becomes 1/10 ^4, the fluid particles at a pressure of 3 trillion atm in view of the present effect or
Or it will shrink the liquid metal . In this case, since the area ratio is 1/10 ⁴ , the initial magnetic field of 50 Tesla is 50 * 10 ⁴
= Concentrated to a magnetic field of 500,000 Tesla. In addition, 500,000 Tesla
Has a magnetic pressure of 1 trillion atmospheres.

This magnetic field concentration process proceeds until the magnetic pressure and the laser light pressure are in equilibrium. When the pulse irradiation of the laser light is completed, the light pressure decreases, so that the contracted fluid particles or liquid metal try to proceed to the expansion and explosion process due to the magnetic pressure. At this point, the superconducting magnet (43, 4
The magnetic field generating action of 4) is stopped. Fluid particles that remain in the blanket 41 after the magnetic flux is frozen by stopping the magnetic field
Alternatively, the liquid metal is exhausted by the exhaust pump 47 and returned to the liquid metal storage container 48 again. In this process, degaussing action is performed if necessary.

The above process is set as one cycle and is repeated several thousand cycles per second. That is, a strong magnetic field of 500,000 Tesla is generated by continuous pulses of several KHz. Then, as described above, the intensities of the left and right laser light sources (45, 46) are controlled. That is, this device is provided with the magnetic energy generating means and the magnetic control means.

The generation of a strong magnetic field of about 500,000 tesla, which is the most viable in the existing technology, has been described above. The strength of the generated magnetic field depends on the laser light power density and the radius ratio obtained by the implosion effect. What is different can be understood from the above description.

That is, this apparatus freezes a magnetic flux of an initial magnetic field of 50 Tesla to 500 Tesla into atomized particles of a highly conductive fluid (liquid metal) or liquid metal , and laser light (power density: 10 ¹⁴ (W / cm ² to 10 ¹⁸ W / cm ² ) By the implosion effect by irradiation, the radius ratio is 1/100 to 1 /
Therefore, the initial magnetic field of 50 Tesla to 500 Tesla is concentrated to 1 / 10,000 to 1 / 100,000,000 times by contracting the fluid of 10,000 to 1 / 10,000 to 1 / 100,000,000 by the area ratio.
It is possible to generate ultra-high magnetic fields of 10,000 to 50 million Tesla to 50 billion Tesla in a pulsed manner.

In addition, spraying of atomized particles or liquid metal
Since the pouring and the laser light irradiation can be controlled mechanically and electrically, continuous pulse operation of several KHz to several tens of MHz can be easily performed. It should be noted that there is no need for a structure such as a liner for concentrating the magnetic field, and there is a feature that the structure is not destroyed by the giant magnetic pressure generated by the magnetic field generation. As a laser light source
Uses an organic dye laser with forced mode locking
This organic dye laser is a powerful pico pulse with high power density.
Because laser can be realized by repeating several MHz to several GHz.
is there.

Table 2 shows the expected main performance specifications of the flying object according to the present invention.

[0295]

[Table 2]

For reference, a book on space-driven propulsion spacecraft
The calculation formula of the body is 100, and the magnetic flux freeze laser implosion engine
The calculation formula of the
21).

[0297]

[Equation 100]

[0298]

[Equation 101]

In the equation 100, R ⁰⁰ : space
Curvature (1 / m ² ), B: Magnetic field (Tesla), c: Light velocity value (space
Strain transfer velocity) (m / s), S: Area length of curved space
(M), L: Spacecraft body length (m), N: Repeated propulsion pulse
Frequency (Hz): = Number of propulsion pulses per second, α
_NET : Net acceleration received by the spacecraft (m / s ² ), τ: Thrust
Effective time (propulsion pulse width) (s), t: Acceleration time (engine
Operating time) (s), M: spacecraft mass (Kg), V: spacecraft
Velocity (m / s), F: Spacecraft thrust (N).

Also, in the equation 101, ε: propulsion pulse
1 cycle (T = 1 / N) laser energy (J), k: conventional
Number of sustaining pulses, ε _s : Ray per inertia maintaining pulse
The irradiation energy (J), S _D : Laser power density (W /
m ² ), t _L : Laser irradiation time (s), A: Laser irradiation area
(M ² ), χ: Implosion radius ratio (<< 1), u: Implosion laser light pressure
(N / m ² : = Pa), P _u : Magnetic pressure (N / m ² : = Pa), E:
Energy supplied per second (J / s: = W): = Engine
The power supply P _E (W).

As an example of calculation, the spacecraft length (direct
Diameter) L = 15 m, curved space area S (= 3 L) = 45
m, magnetic field B = 80 billion Tesla
Shown below. Start study on laser implosion engine
It is just after, and I would like to keep it as a guide only. τ =
t ₂ = L / c = 50 ns, t ₁ = S / c = 150 ns, t ₃ = 0 ns.
Set the Max value of N = 1 / t ₁ , N = 6.7MHz. R ⁰⁰ = 5.3 × 10 ^-16 (1 / m ² ), α = 2146 m / s ² = 219G, α
_NET = 36G. P _u = 2.5 × 10 ²⁷ Pa. ε = 10MJ, k = 10, t _L = 0.1P
s, A = 0.0314 cm ² , χ = 0.2 × 10 ⁻⁵ , S _D = 3.
2 × 10 ²⁴ W / m ² , u = 2.7 × 10 ²⁷ Pa, and u ≈ P _u .
It E = P _E = 67 TW. Maximum propulsion acceleration of one engine 36G, power supply 67T
W. Spacecraft Propulsion direction 3 engines Maximum propulsion acceleration 10
8G, power supply 200 TW. Spacecraft speed and thrust
To control the force, lower the propulsion pulse repetition frequency N
And reduce the propulsion acceleration from 108G to 36G to 1G to 0G.
You can For example, in the case of 1G, the height of the spacecraft
L = 5 m, curved space region S = L = 5 m, magnetic field 800
100 Tesla, N = 4.9MHz, τ = t ₂ = L / c = 17ns,
_{t 1 = S / c = 17ns} , t 3 = 170ns, R 00 = 5.3 × 10
^-16 , α = 236m / s ² = 24G, α _NET = 1G, E = P _E = 4.
It becomes 9TW. Power is 0.01 ps (10 f _S ) for laser irradiation time t _L
If set to, both calculation examples will be 1/10.

Note that the power required for the propulsion device is generated.
As a power source for this, liquid gold that is small and can take out a large current is used.
Genus MHD generator (MHD power generation using liquid metal as working fluid
Machine), the pair annihilation reaction between antiproton and proton is used as the heat source.
The anti-particle annihilation reactor used is used.

[0303]

As described above, the flying object of the present invention
According to the propulsion device, the propulsive force of the flying object is
Volume force (spatial strain) equivalent to gravity that permeates the entire space
Force), and everything including the flight vehicle and the crew inside the flight vehicle.
The mass point receives the same force and is accelerated, and the
There is no need to use it, and crew members will not be destroyed.

This is a propulsion method that theoretically eliminates inertial force,
Therefore, from the stationary state in the air, sudden starts and sudden starts in all directions.
Arbitrary navigation such as stop, right-angled turn, zigzag turn and V-turn
Law becomes possible.

Further, since the propulsive force is equivalent to gravity,
In principle, the final speed is around the light speed (quasi-light speed).
Is possible.

Furthermore, the propulsion device of the present invention is used in an internal combustion engine.
There is no noise (propeller sound, gas injection sound, etc.)
Quiet flight is possible without generating noise. Also, the navigation
Stable (stationary in the air ~ low speed ~ high speed is optional), explosion
It is highly safe because it does not carry the fuel that is a matter of nature.

[0307] In addition, the propulsive force is the entire space area including the flying object.
Since it acts on the body, the air on the outer surface of the flying body is also accelerated.
Therefore, the occurrence of aerodynamic heating can be reduced. Tsuma
It is only friction between air molecules and air molecules,
High-speed flying objects in the atmosphere (several km / s to several 100 km / s)
You can move with.

From the above, it is possible to navigate the outer space at quasi-light speed.
Ability to go and high speed in the air with any flight pattern
Expecting various excellent effects in combination with the ability to navigate
Furthermore, shortening of navigation time for planetary exploration (for example, to Mars)
One way half day) has a great effect.

[Brief description of drawings]

FIG. 1 is an explanatory diagram of a basic structure of a space.

FIG. 2 is an explanatory diagram of a surface force difference as a driving force.

FIG. 3 shows an appearance of a flying object according to an embodiment of the present invention,
(A) is a schematic top sectional view, and (B) is a schematic side sectional view.

FIG. 4 is an explanatory view of the principle of the spatial distortion propulsion mechanism.

FIG. 5 is a layout view of four propulsion engines.

[6] Ri navigation illustration Der by propulsion engines of six or four, the (A) is sudden acceleration and stopping from hover shows
However, (B) shows a right-angled turning flight, and (C) shows a zigzag flight.
Indicates a line.

FIG. 7: Spatial distortion around the earth and the object M in this space
FIG.

FIG. 8 is an object M in the case where there is no mass body such as the earth and there is a unidirectional spatial distortion similar to the space around the earth.
FIG.

FIG. 9 is an explanatory diagram of a propulsion principle of the present invention.

FIG. 10 is an explanatory diagram of an ideal space distortion surface for propelling a spacecraft.

FIG. 11 is an explanatory view of a practical space distortion surface for propelling a spacecraft.

FIG. 12 is an explanatory view of a practical space distortion surface for propelling a spacecraft.

FIG. 13 is an explanatory diagram of the arrangement of propulsion engines and the motility of the spacecraft, (A) shows the case of six engines,
(B) shows the type of engine, (C) shows the case of four engines.

FIG. 14 is an explanatory diagram of a spatially strained surface formed by one superconducting magnet.

FIG. 15 is an explanatory diagram of the principle structure of the propulsion engine of the present invention.

FIG. 16 is an explanatory diagram of a spatial distortion surface formed by the propulsion engine of the present invention.

FIG. 17 is a conceptual diagram of magnetic field concentration by magnetic flux freezing,
(A) is a state diagram in which the magnetic flux is frozen in the highly conductive fluid particles,
(B) is a state diagram in which the fluid particles are contracted by the action of an external force and the magnetic flux is also contracted accordingly, and (c) is a state diagram in which the fluid particles are further contracted.

FIG. 18 is a principle explanatory diagram of a strong magnetic field generator according to an embodiment of the present invention.

FIG. 19 is a configuration block diagram of a strong magnetic field generator according to an embodiment of the present invention.

FIG. 20 is an operation state diagram according to ON / OFF of the engine.
is there.

FIG. 21 is an explanatory diagram of operation pulses.

[Explanation of Codes] 1 Flying body 21-26 Propulsion engine 31 Main superconducting magnet 32 Auxiliary superconducting magnet 41 Blanket 42 Nozzle 43-44 Superconducting magnet 45-46 Laser light source 47 Exhaust pump 48 Liquid metal storage container

[Procedure Amendment 2]

[Document name to be corrected] Drawing

[Name of item to be corrected] Fig. 17

[Correction method] Change

[Correction content]

FIG. 17

[Procedure 3]

[Document name to be corrected] Drawing

[Name of item to be corrected] Fig. 20

[Correction method] Added

[Correction content]

FIG. 20

[Procedure amendment 4]

[Document name to be corrected] Drawing

[Correction target item name] Fig. 21

[Correction method] Added

[Correction content]

FIG. 21

Claims (3)

[Claims] 1. Magnetic energy generating means for generating a strong magnetic field for changing a curvature component of a space inside a flying object (aircraft, manned rocket, spacecraft, etc.) and a space around the flying object; By controlling the generation mode of the strong magnetic field by the means, the change of the curvature component of the space is locally controlled quasi-antisymmetrically, and the spatial distortion force equivalent to the gravity generated in the space is used as the propulsive force of the flying object. And a magnetic control means for controlling the propelling device for the flying object. 2. The flying vehicle propulsion device according to claim 1, wherein the magnetic energy generating means is a main superconducting magnet that generates a spherical magnetic field and is arranged inside a spherical body made of a superconducting material. The magnetic control means arranges an auxiliary superconducting magnet that generates a magnetic field of opposite polarity in a hemispherical magnetic field on one side of the main superconducting magnet,
A propulsion device for a flying object, characterized by changing and controlling a repetition frequency of exciting current pulses of both superconducting magnets. 3. The flying vehicle propulsion device according to claim 1, wherein the magnetic energy generating means includes a liquid metal storage container that stores liquid metal that is a highly conductive fluid; and a spherical blanket that is a strong magnetic field generating container. A nozzle for injecting liquid metal from the liquid metal storage container into the blanket as atomized fluid particles; and a pair of nozzles arranged to face opposite wall portions of the blanket to generate an initial magnetic field in the blanket. Superconducting magnet;
A pair of laser light sources that are arranged to face the blanket wall portions on both sides orthogonal to the arrangement direction of the pair of superconducting magnets and irradiate pulsed laser light to fluid particles whose magnetic flux is frozen;
An exhaust pump for returning the fluid particles whose magnetic flux is defrosted to the liquid metal storage container; the magnetic control means controls an exciting current to the pair of superconducting magnets; and the pair of laser light sources. Asymmetrical control and control of repeating the process from the injection of fluid particles to the exhaust at high speed; and the like.